2019 - Satellite & Spacecraft Launches and Detailed Orbits

Listed are all launches, irrespective of outcome, that were irretrievably committed to flight towards orbit or intended to accelerate the payload to escape velocity.

Launch times are in UTC and are from the launching agency or estimated by 'walking back' along the ground track to the launch site. The PRIME source of orbit data and decay information is SpaceTrack. All other major sources draw heavily on the Space-Track data.

To fill the gaps where Space-Track's elements are not published because they have a classification of "Secret", a minority of orbits is based on amateur observations using visual and radio techniques. Such data is published near-daily by Mike McCants and the source observations can often be found in the web-based Seesat-L discussion group. Occasionally, early orbit data are published by satellite owners and may cover periods before SpaceTrack lists a new object. In extreme cases, orbits are estimated from public data.

Apogee and perigee are measured against a spherical Earth situated at the focus of the orbital ellipse and with a radius of 6378.145 km. Care should be exercised when comparing with other published orbits even when the source is shown as SpaceTrack because they may be be based on a different model.

Web sites may link to specific launches by pointing to the page URL followed by the three digit launch number, eg - http://www.zarya.info/Diaries/Launches/Launches.php?year=2019#001

2019-022 Antares 230 Wallops Flight Facility						2019 Apr 17, 20:46
SS Roger Chaffee (Cygnus NG-11) 2019-022A 44188					Re-entered - 2019 Dec 6 Life 233 days
Northrop Grumman vehicle carrying supplies to ISS. Captured by RMS Remote Manipulator Apr 19, 0928 UTC, docked with downward- facing port of Unity at 11:31 UTC. Undocked Aug 6 at 13:30 UTC, released from Remote Manipulator at 16:15 UTC. Launched several Cubesats after departing ISS. Destructive re-entry above the southern Pacific Ocean 2019 Dec 6, probably at around 16:55 UTC followed retrofire about 40 minutes earlier.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Apr 17, 22:24	6711	0.0071	285	380	91.18	51.64	305
2019 Apr 18, 20:48	6780	0.0002	401	403	92.60	51.63	228
2019 Apr 18, 22:21	6782	0.0001	403	404	92.64	51.64	85
2019 Apr 19, 07:52	6783	0.0007	400	410	92.67	51.69	119
2019 Apr 19, 12:21	6787	0.0001	408	410	92.75	51.64	194
2019 Aug 05, 05:22	6792	0.0006	409	418	92.84	51.64	219
2019 Aug 06, 20:59	6825	0.0047	415	479	93.52	51.63	318
2019 Aug 06, 22:33	6853	0.0050	440	509	94.10	51.66	8
2019 Aug 16, 22:23	6853	0.0012	466	483	94.09	51.64	294
2019 Sep 16, 11:48	6852	0.0014	465	484	94.09	51.64	45
2019 Sep 17, 09:43	6842	0.0006	459	468	93.86	51.64	309
2019 Oct 08, 18:30	6844	0.0006	462	470	93.92	51.63	352
2019 Oct 18, 12:53	6794	0.0007	411	421	92.89	51.64	160
2019 Oct 20, 18:19	6844	0.0006	462	470	93.91	51.63	38
2019 Dec 01, 22:20	6844	0.0005	462	469	93.91	51.63	177

Antares upper stage 2019-022B 44206					Re-entered - 2019 Apr 28 Life 11 days
Launched SS Roger Chaffee (Cygnus NG-11). Initial orbit not published by Space-Track but probably approx 190 x 275 km.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Apr 24, 15:25	6588	0.0032	188	230	88.68	51.61	166

2019-I08 Nanoracks Cubesat Deployer International Space Station						2019 Jul 3, 10:15
GEMS (Global Environmental Monitoring System) 1998-067QK 44385					in space
3U Cubesat equipped with microwave radiometer i to capture 3D temperature and moisture atmospheric profiles. IOD (In Orbit Demonstration System) launch from Orbital Micro Systems.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 09, 18:42	6790	0.0004	409	414	92.80	51.64	119

2019-I09 Nanoracks Cubesat Deployer International Space Station						2019 Jul 3, 11:50
KRAKsat 1998-067QL 44426					in space
1U Cubesat - produced students at the AGH University of Science and Technology, Kraków, carrying an experiment to investigate the use of ferrofluid (powdered metal) as a flywheel. Its storage batteries failed to hold a charge from the the solar cells.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 14, 06:55	6790	0.0006	408	416	92.80	51.65	114

Światowid 1998-067QM 44427					in space
2U Cubesat from Poland, carrying a high resolution Earth imaging system.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 13, 20:06	6790	0.0005	409	415	92.81	51.64	126

2019-I10 Nanoracks Cubesat Deployer International Space Station						2019 Jul 3, 14:50
VCC A (Virginia Cubesat Constellation A) 1998-067QN 44428					in space
1U Cubesat - One of a set of three launched simultaneously to provide measurements of orbit decay. Each was equipped with a drag device to cause re-entry at the end of mission. Built by a consortium of universities in the state of Virginia, USA. All three reportedly failed to activate on release into orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 14, 17:42	6790	0.0003	409	414	92.79	51.64	140

VCC C (Virginia Cubesat Constellation C) 1998-067QQ 44430					in space
1U Cubesat - One of a set of three launched simultaneously to provide measurements of orbit decay. Each was equipped with a drag device to cause re-entry at the end of mission. Built by a consortium of universities in the state of Virginia, USA. All three reportedly failed to activate on release into orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 13, 21:37	6790	0.0003	409	414	92.79	51.64	140

VCC B (Virginia Cubesat Constellation B) 1998-067QR 44431					in space
1U Cubesat - One of a set of three launched simultaneously to provide measurements of orbit decay. Each was equipped with a drag device to cause re-entry at the end of mission. Built by a consortium of universities in the state of Virginia, USA. All three reportedly failed to activate on release into orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 14, 13:05	6790	0.0004	409	414	92.80	51.64	148

2019-I11 Nanoracks Cubesat Deployer International Space Station						2019 Jul 3, 16:25
Entrysat 1998-067QP 44429					in space
3U Cubesat from ISAE-SUPAERO and funded by CNES, France - inert satellite designed to study the behaviour of a piece of space debris in orbit and approaching re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 14, 16:10	6789	0.0003	409	414	92.79	51.64	137

2019-038 Soyuz-2 1B + Fregat Vostochny Cosmodrome						2019 Jul 5, 05:41
Meteor M2-2 2019-038A 44387					in space
Meteorological satellite providing global observations of the Earth's surface and its atmosphere. The data acquired by the satellite is used for weather analysis and forecasting, climate change monitoring, sea water monitoring and forecasting, and space weather analysis and prediction.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Jul 05, 21:02	7192	0.0003	812	816	101.17	98.57	85	03:05
2019 Dec 17, 20:21	7192	0.0001	813	815	101.17	98.59	5	02:58
2019 Dec 18, 11:32	7191	0.0002	811	815	101.15	98.59	62	02:58

2019-040 Proton-M + DM-3 Baikonur Cosmodrome		2019 Jul 12, 12:30
Spektr RG (Spektr Roentgen-Gamma) 2019-040A 44432	in space
Joint Russian and German high-energy astrophysics observatory carrying a German x-ray telescope to map galaxy clusters, and a Russian x-ray telescope to search for supermassive black holes. Arrived L-2 2019 Oct 21.
Halo orbit around the Sun-Earth L-2 Lagrange Point

DM-3 rocket stage 2019-040B 44433	in space
Launched Spektr RG.
Heliocentric orbit

2019-041 Soyuz FG Baikonur Cosmodrome						2019 Jul 20, 16:28
Soyuz MS-13 (Soyuz 11F732A48 № 743) 2019-041A 44437					Re-entered - 2020 Feb 6 Life 201 days Returned to Earth
Carrying crew to ISS - Alexandr Skortsov (Roscosmos), Luca Parmatiano (ESA) and Andrew Morgan (NASA). Precise launch time 16:28:21 UTC. Docked with the aft port of Zvezda Jul 20 at 22:47:50 UTC. Undocked, carrying its original crew, Aug 26 at 03:35 UTC and re-docked under manual control with the Poisk module at 03:59 UTC in order to allow Soyuz MS-14 to use Zvezda after its aborted docking with Poisk. Undocked 2020 Feb 6, 08:50 UTC carrying Skortsov, Parmatiano and Christina Koch (NASA). Retro-fire at 08:18 OTC led to landing shortly before 09:13 UTC approx 150 km SE of Dzhezkazgan in Kazakhstan.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 20, 18:31	6641	0.0009	257	269	89.77	51.60	72
2019 Jul 20, 21:04	6792	0.0007	409	418	92.84	51.64	161

Soyuz upper stage 2019-041B 44438					Re-entered - 2019 Jul 24 Life 4 days
Launched Soyuz MS-13.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 20, 20:41	6577	0.0005	196	202	88.47	51.61	87

2019-042 GSLV Mk III M1 Satish Dhawan Space Centre						2019 Jul 22, 09:13
Vikram Lunar Lander					in space
Indian lunar landing vehicle carrying 'Pragyan' lunar rover. Separated from Chandrayaan 2 Sep 2 at 0745 UTC. Three retro-firings Sep 3 at 03:20 UTC and 22:12 UTC, and Sep 6 at 20:08 UTC set it on course for landing but it crashed on the lunar surface at 20:23 UTC.
Impacted on the Moon

Chandrayaan 2 2019-042A 44441					Re-entered - 2019 Sep 6 Life 46 days
Indian lunar orbiter, carried 'Vikram' lunar lander. Used five engine firing starting Jul 24 to raise its orbit before entering Barycentric orbit Aug 13. Retro-fire Aug 20 at 03:32 UTC placed it into lunar orbit. Four further firings lowered the orbit to operational height for release of Vikram on Sep 2. Chandrayaan then began its own lunar exploration mission from orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 24, 05:28	29046	0.7758	133	45203	821.08	21.43	179
2019 Jul 26, 15:10	33860	0.8057	202	54762	1033.47	21.42	181
2019 Aug 01, 20:31	42280	0.8409	348	71456	1442.00	21.06	183
2019 Aug 06, 09:36	51042	0.8699	264	89064	1912.72	21.56	185
2019 Aug 13, 21:07	78528	0.9148	313	143986	3650.00	21.67	186
2019 Aug 18, 00:00	208216	0.9751	-1201	404877	15759.08	21.81	184

GSLV upper stage 2019-042B 44442					Re-entered - 2019 Oct 16 Life 86 days
Launched Chandrayaan 2.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 24, 23:02	29034	0.7753	145	45167	820.57	21.41	180

2019-043 Hyperbola 1 Jiuquan Space Centre						2019 Jul 25, 05:00
CAS 7B + BP-1B (China Amateur radio Satellite) 2019-043A 44443					Re-entered - 2019 Aug 6 Life 12 days
1.5U Cubesat - combined payload consisting of an amateur radio transponder package and telemetry transmitter (CAS-7B) and a balloon experiment to increase air drag and accelerate orbit decay (BP-1B).
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 25, 15:38	6668	0.0014	280	299	90.31	42.72	279

Hyperbola 1 (SQX-1) upper stage					Re-entered - 2019 Jul 25 Life <1 day
Launched CAS-7. Also carried three experimental payloads that remained attached to it alongside two ballast items carrying commercial advertisements. Re-entered soon after releasing satellite and not catalogued.
Not Catalogued - orbit parameters unavailable

2019-044 Falcon 9 Block 5 Cape Canaveral						2019 Jul 25, 22:01
SpaceX Dragon CRS-18 2019-044A 44446					Re-entered - 2019 Aug 27 Life 33 days Returned to Earth
Carrying a cargo to ISS under NASA's Commercial Resupply Services (CRS) contract. Captured by the ISS Remote Manipulator System July 27 at 13:11 UTC and attached to the lower port of the Harmony module at 16:01 UTC. Undocked using the RMS Aug 27 at 12:25 UTC. Released 14:59 UTC. Retro-fire led to splashdown at 20:20 UTC in the Pacific Ocean, about 300 km SW of Baja, California.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 26, 00:59	6673	0.0138	203	387	90.41	51.63	49
2019 Jul 26, 23:34	6666	0.0127	203	373	90.28	51.64	53
2019 Jul 27, 05:34	6664	0.0126	203	370	90.24	51.65	54
2019 Jul 27, 13:31	6792	0.0006	409	418	92.84	51.64	184
2019 Aug 27, 12:22	6794	0.0008	410	421	92.88	51.64	333
2019 Aug 27, 17:12	6784	0.0013	397	414	92.67	51.65	283

Falcon 9 upper stage					Re-entered - 2019 Jul 25 Life <1 day
Launched Dragon CRS-18. Caused to re-enter soon after releasing payload, not catalogued.
Not Catalogued - orbit parameters unavailable

2019-045 CZ 2C Xichang Space Centre						2019 Jul 26, 03:57
Yaogan-30 13 2019-045A 44449					in space
One of a triplet of simultaneously-launched satellites described as being for "electromagnetic environment detection and related technological tests”. That may indicate they are electronic intelligence gathering satellites. The three satellites are spaced at 120º intervals around the orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 26, 15:38	6975	0.0012	588	605	96.62	35.00	304
2019 Jul 31, 12:13	6985	0.0007	602	611	96.82	35.00	328
2019 Aug 15, 03:15	6977	0.0004	596	602	96.67	35.00	318

Yaogan-30 14 2019-045B 44450					in space
One of a triplet of simultaneously-launched satellites described as being for "electromagnetic environment detection and related technological tests”. That may indicate they are electronic intelligence gathering satellites. The three satellites are spaced at 120º intervals around the orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 26, 17:56	6975	0.0011	589	605	96.62	35.00	302
2019 Jul 29, 18:55	6976	0.0010	591	605	96.64	35.00	325
2019 Aug 12, 00:43	6977	0.0010	592	606	96.66	34.99	84

Yaogan-30 15 2019-045C 44451					in space
One of a triplet of simultaneously-launched satellites described as being for "electromagnetic environment detection and related technological tests”. That may indicate they are electronic intelligence gathering satellites. The three satellites are spaced at 120º intervals around the orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 26, 17:56	6975	0.0011	589	604	96.61	35.00	302
2019 Jul 30, 16:45	6967	0.0009	583	595	96.45	35.00	336
2019 Aug 14, 08:29	6977	0.0001	598	600	96.67	35.00	145

CZ 2C upper stage 2019-045D 44452					in space
Launched cluster of three Yaogan-30 satellites. Perigee lowered after satellite release.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 28, 18:49	6903	0.0103	454	597	95.14	34.98	65

2019-I07 Dextre Arm + Kaber Micro Satellite Deployer International Space Station						2019 Jul 27, 20:05
RedEye 1 (Pinot) 1998-067QJ 44364					in space
Small satellite from DARPA, possibly for testing inter-satellite communication links.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jun 28, 09:21	6791	0.0008	407	418	92.82	51.64	85

2019-046 Soyuz-2 1A + Fregat Baikonur Cosmodrome						2019 Jul 30, 05:57
Meridian 8 (Meridian № 18L) 2019-046A 44453					in space
HEO military/government comsat to support Russian forces, commercial shipping and communication ground stations at northern latitudes across Russia. First mission for the Meridian-M version. Meridian also supports the clandestine short messaging system formerly provided by the Parus satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 01, 14:38	26738	0.7246	985	39734	725.19	62.81	270
2019 Aug 19, 14:00	26555	0.7225	990	39364	717.76	62.79	270

Fregat rocket stage 2019-046B 44454					in space
Launched Meridian 8.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 09, 05:05	26575	0.7297	805	39588	718.56	62.75	270

Soyuz upper stage					Re-entered - 2019 Jul 30 Life <1 day
Launched Meridian 8. Re-entered naturally over southern Indian Ocean about 1 hr after launch before completing first orbit.
Not Catalogued - orbit parameters unavailable

2019-047 Soyuz-2 1A Baikonur Cosmodrome						2019 Jul 31, 12:10
Progress MS-12 (Progress 7K-TGM №442) 2019-047A 44455					Re-entered - 2019 Nov 29 Life 121 days
Supplies to ISS. Precise launch time 12:10:46 UTC. Docked with the port on Pirs 2019 Jul 21 at 15:29 UTC. Undocked 2019 Nov 28 at 10:25 UTC. Retro-fire at 13:39 UTC led to destructive re-entry above the southern Pacific Ocean at 14:11 UTC. Any surviving fragments hit the ocean surface about eight minutes later.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 31, 07:53	6792	0.0006	409	418	92.84	51.64	199

Soyuz upper stage 2019-047B 44456					Re-entered - 2019 Aug 4 Life 4 days
Launched Progress MS-12.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Jul 31, 22:19	6578	0.0022	185	215	88.50	51.61	69

2019-048 Proton-M + Briz-M Baikonur Cosmodrome						2019 Aug 5, 21:56
Cosmos 2539 (Blagovest, 14F149 № 14L) 2019-048A 44457					in space
Russian military and civilian communications satellite providing high-speed internet, data communications, television and radio broadcasting, telephony and videoconferencing services.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Aug 13, 23:08	42102	0.0027	35610	35837	1432.87	0.04	306	63° east
2019 Aug 15, 18:13	42143	0.0021	35676	35854	1435.01	0.03	309	64° east
2019 Aug 16, 13:10	42158	0.0017	35707	35853	1435.74	0.03	303	64° east
2019 Aug 21, 07:12	42281	0.0008	35867	35938	1442.02	0.01	121	60° east
2019 Aug 30, 11:19	42197	0.0006	35793	35846	1437.76	0.01	326	45° east
2019 Aug 30, 22:25	42179	0.0004	35785	35816	1436.81	0.01	290	45° east
2019 Aug 31, 04:30	42177	0.0004	35780	35818	1436.73	0.02	294	45° east

Briz-M rocket stage 2019-049B 44458					in space
Launched Cosmos 2539. Orbit raised after releasing the satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 21, 17:56	45223	0.0712	35625	42066	1595.16	0.16	157

Briz-M propellant tank 2019-049C 44459					in space
Auxilliary propellant tank discarded by Briz-M that launched Cosmos 2539.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 17, 17:29	24429	0.7229	390	35711	633.30	48.71	3

2019-049 Ariane 5ECA Cape Canaveral						2019 Aug 6, 19:30
EDRS-C (European Data Relay Satellite) 2019-049A 44475					in space
Second satellite in EDRS to provide point to point communications including to/from other satellites including the ISS. Brought into service 2020 Jan 23.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Aug 08, 08:02	24400	0.7291	232	35812	632.19	4.47	179
2019 Aug 13, 09:32	39141	0.0775	29730	35797	1284.44	0.16	194
2019 Aug 14, 07:39	40657	0.0371	32770	35787	1359.75	0.13	180
2019 Aug 16, 04:20	42154	0.0003	35765	35787	1435.54	0.07	353	18° east
2019 Aug 19, 00:57	42073	0.0008	35661	35729	1431.42	0.08	195	19° east
2019 Aug 23, 05:11	42141	0.0006	35738	35787	1434.89	0.10	358	22° east
2019 Aug 25, 20:57	42165	0.0001	35784	35789	1436.09	0.09	222	21° east
2019 Nov 26, 20:02	42164	0.0001	35782	35788	1436.03	0.04	324	21° east
2019 Nov 27, 05:58	42069	0.0001	35688	35694	1431.21	0.04	71	22° east
2019 Dec 06, 21:59	42165	0.0001	35783	35791	1436.12	0.01	250	31° east

Intelsat 39 2019-049B 44476					in space
Commercial comsat providing video distribution and broadband connections to customers across Africa, Asia, Europe, the Middle East and Asia. Expected location - 29° east to replace Intelsat 902.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Aug 08, 10:58	26530	0.5889	4527	35776	716.73	2.86	178
2019 Aug 10, 02:44	30590	0.3781	12647	35776	887.41	1.55	177
2019 Aug 11, 23:48	41078	0.0257	33645	35754	1380.92	0.38	172
2019 Aug 19, 18:14	41266	0.0234	33923	35853	1390.43	0.38	171
2019 Aug 27, 00:46	42199	0.0006	35794	35848	1437.86	0.11	297	78° east
2019 Aug 29, 14:24	42177	0.0006	35775	35822	1436.71	0.05	29	55° east
2019 Sep 26, 05:05	42165	0.0001	35783	35791	1436.12	0.03	49	55° east
2019 Sep 30, 19:19	42095	0.0001	35713	35721	1432.53	0.04	30	59° east
2019 Oct 04, 20:16	42113	0.0004	35719	35752	1433.48	0.03	242	62° east
2019 Oct 07, 20:24	42163	0.0001	35781	35790	1436.03	0.03	105	62° east

Ariane 5 upper stage 2019-049C 44477					in space
Launched Intelsat 39 and EDRS-C
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 08, 18:39	24251	0.7280	217	35528	626.40	4.55	181

2019-050 Falcon 9 Block 5 Cape Canaveral						2019 Aug 6, 23:23
Amos 17 2019-050A 44479					in space
Israeli comsat covering Africa, Europe and the Middle East. Expected location - 17° east.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Aug 08, 05:56	24354	0.7292	217	35734	630.39	26.01	178
2019 Aug 10, 14:40	25907	0.6266	3295	35763	691.65	16.69	179
2019 Aug 12, 11:58	33372	0.2631	18214	35774	1011.20	4.02	178
2019 Aug 12, 20:22	38964	0.0818	29399	35773	1275.71	0.95	173
2019 Aug 15, 04:11	41705	0.0112	34861	35793	1412.68	0.09	94	12° east
2019 Aug 15, 17:58	42273	0.0020	35809	35979	1441.61	0.17	305	14° east
2019 Aug 19, 15:00	42166	0.0002	35781	35794	1436.15	0.17	292	14° east

Falcon 9 upper stage 2019-060B 44480					in space
Launched Amos 17.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 08, 02:22	24342	0.7292	214	35714	629.95	26.03	178

2019-051 Atlas V 551 Cape Canaveral						2019 Aug 8, 10:13
USA 292 (AEHF 5) 2019-051A 44481					in space
Advanced Extremely High Frequency US military and government communications satellite. Lift-off was 29 minutes into the launch window after a short delay. Separated from the launch vehicle at 15:53 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Aug 09, 15:38	31204	0.3352	14366	35287	914.29	9.99	180
2019 Aug 11, 16:08	33218	0.2749	17709	35971	1004.22	9.48	180
2019 Aug 13, 11:30	34686	0.2013	21327	35290	1071.51	8.63	181
2019 Aug 16, 23:19	36458	0.1430	24865	35295	1154.65	8.15	181
2019 Aug 28, 15:15	36812	0.1280	25723	35146	1171.52	7.91	180
2019 Sep 09, 18:00	37412	0.1052	27098	34970	1200.27	7.71	179
2019 Oct 22, 20:51	40258	0.0492	31900	35859	1339.78	6.97	182
2019 Nov 04, 03:15	41441	0.0365	33549	36577	1399.28	6.76	186
2019 Nov 07, 13:09	41741	0.0322	34017	36708	1414.49	6.70	185	119° west
2019 Nov 11, 23:43	41997	0.0226	34670	36569	1427.55	6.59	185	99° west
2019 Nov 22, 22:27	42167	0.0004	35773	35804	1436.19	6.40	293	94° west

TDO 1 2019-051B 44482					in space
12U Cubesat (4x3) - possibly equipped with laser reflectors for visual tracking. Purpose is for calibration of laser-based tracking equipment on the ground.. Separated from launch vehicle at 10:42 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 28, 12:00	24124	0.7268	213	35278	621.49	26.26	193

Atlas V upper stage (Centaur) 2019-051C 44483					in space
Launched AEHF 5 and TDO 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 23, 02:03	30961	0.3466	13853	35313	903.62	9.66	182

2019-052 Jielong 1 Jiuquan Space Centre						2019 Aug 17, 04:11
Qiancheng 1(?) 2019-052A 44486					in space
Small imaging satellite for remote sensing, particularly for soil moisture monitoring from Qiansheng Exploration Technology Co. Catalogue number and designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Aug 18, 21:28	6924	0.0020	532	559	95.56	97.61	245	10:29

Tianqi 2 2019-052B 44487					in space
Comsat providing messaging communication links from LEO including between Internet-connected items. Catalogue number and designation to be confirmed,
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 18, 21:04	6922	0.0021	529	559	95.53	97.61	251

Xingchidai 5(?) 2019-052C 44488					in space
Small Earth observation satellite owned by Chengdu Guoxing Aerospace Technology Co . Catalogue number and designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 18, 21:04	6923	0.0023	529	560	95.54	97.61	248

Jielong 1 upper stage					Re-entered - 2019 Aug 17 Life <1 day
Launched group of three satellites. De-orbited
Not Catalogued - orbit parameters unavailable

2019-053 CZ 3B Xichang Space Centre						2019 Aug 19, 12:03
Chinasat 18 2019-053A 44493					in space
Comsat intended for geosynchronous orbit. Problems detected soon after separation from the launch vehicle left it stranded in useless transfer orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 20, 19:12	24383	0.7292	224	35785	631.50	28.40	180

CZ 3B upper stage 2019-053B 44494					in space
Launched Chinasat 18.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 20, 03:38	23659	0.7230	176	34387	603.62	28.41	179

2019-054 Electron Rocket Lab LC-1, New Zealand						2019 Aug 19, 12:12
Galaxy 30 (Galaxy 14R)					in space
Comsat to provide high-performance broadcast distribution, including Ultra-High Definition (UHD) and over-the-top (OTT) streaming media, while also supporting broadband, mobility and enterprise network solutions. Will replace Galaxy 14 (2005-030A/2020 Jul 30). Expected location - 125° west.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude

BSAT-4b					in space
Japanese broadcast comsat providing high definition television services. Will act as backup to, and to supplement, BSat-4A (42951/2017-059B). Expected location - 110°east.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude

MEV-2 (Mission Extension Vehicle 2)					in space
Northrop Grumman spacecraft - launched to rendezvous and attach itself to the Intelsat 10-01 GEO comsat (26766/2001-019A) then take over its pointing and station-keeping functions in order to extend its on-orbit life by five years. May then move to another satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude

BRO-1 (Breizh Reconnaissance Orbiter 1) 2019-054A 44495					in space
6U Cubesat (3x2) for signal intelligence (SIGINT) reporting, specifically for maritime and airborne traffic.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 21, 17:25	6799	0.0186	295	548	93.00	45.01	252

Pearl White 1 2019-054C 44497					in space
6U Cubesat (3x2) - one of a simultaneousl-launched pair on a demonstration mission for USAF Space Command to test new concepts for power, propulsion, communications and controlling air drag. Aimed at one year lifetime, built by Tiger Innovations, Inc.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 21, 20:25	6920	0.0012	534	550	95.48	45.01	283

Pearl White 2 2019-054D 44498					in space
6U Cubesat (3x2) - one of a simultaneousl-launched pair on a demonstration mission for USAF Space Command to test new concepts for power, propulsion, communications and controlling air drag. Aimed at one year lifetime, built by Tiger Innovations, Inc.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 21, 20:25	6919	0.0013	533	550	95.47	45.01	281

Global-4 2019-054E 44499					in space
Commercial multi-spectral Earth imaging satellite from BlackSky Global inc.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 21, 20:26	6922	0.0010	537	550	95.51	45.01	285

Ariane 5 upper stage					in space
Launched Galaxy 30, MEV-2 and BSAT-4b.


Electron kick stage 2019-054B 44496					in space
Launched group of four satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 21, 20:27	6923	0.0009	539	550	95.54	45.01	285

Electron upper stage 2019-054F 44500					in space
Launched group of four satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 26, 20:20	6799	0.0185	295	547	92.99	45.01	282

2019-055 Soyuz-2 1A Baikonur Cosmodrome						2019 Aug 22, 03:38
Soyuz MS-14 (Soyuz 11F732A48 № 744) 2019-055A 44504					Re-entered - 2019 Sep 6 Life 15 days Returned to Earth
Visit to ISS - carried no crew in a test flight with the Soyuz-2 1a launch vehicle. Precise launch time 06:38:31 UTC. Scheduled automatic docking Aug 24 at 05:32 UT with the Pirs module of ISS was called off when a fault was detected in the Kurs rendezvous system aboard Pirs during the approach. Soyuz MS-14 stood off from the ISS while Aleksandr Skvortsov, Luca Parmitano and Andrew Morgan boarded Soyuz MS-13 and relocated the craft from Zvezda to Pirs using manual control. Soyuz MS-14 docked automatically with the rear port of Zvezda Aug 27 at 03:12 UTC. Undocked 2019 Sep 7 at 18:14 UTC. Retro-fire at 20:37 UTC led to landing in Kazakhstan at 21:32 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 22, 05:39	6588	0.0024	194	226	88.70	51.65	75
2019 Aug 23, 12:49	6670	0.0009	286	297	90.35	51.64	324
2019 Aug 24, 03:29	6667	0.0006	285	293	90.29	51.63	332
2019 Aug 24, 09:53	6795	0.0006	413	420	92.90	51.64	319
2019 Aug 26, 11:39	6794	0.0004	414	418	92.89	51.64	320
2019 Aug 28, 09:57	6794	0.0008	410	421	92.88	51.65	337

Soyuz upper stage 2019-055B 44505					Re-entered - 2019 Aug 26 Life 4 days
Launched Soyuz-MS-14.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 22, 04:09	6584	0.0015	195	216	88.61	51.65	65

2019-056 Delta 4 Medium+ (5,2) Rocket Lab LC-1, New Zealand						2019 Aug 22, 13:06
USA 293 (GPS IIIA SV02, Magellan) 2019-056A 44506					in space
Block 3 GPS Navsat.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 23, 03:04	17063	0.5561	1195	20174	369.69	55.01	270
2019 Aug 29, 16:33	25325	0.0488	17712	20181	668.47	55.02	270
2019 Sep 03, 21:36	26567	0.0002	20183	20195	718.24	55.02	130

Delta 4 upper stage					Re-entered - 2019 Aug 22 Life <1 day
Launched USA 296. De-orbited soon after releasing satellite, not catalogued.
Not Catalogued - orbit parameters unavailable

2019-057 Rokot + Briz-KM Baikonur Cosmodrome						2019 Aug 30, 14:00
Cosmos 2540 (Geo-IK-2 № 13/Musson 2-3) 2019-057A 44517					in space
Geodetic satellite, based on the GLONASS-M chassis with equipment including radar altimeter, laser retro reflectors and GLONASS receivers. Final use of Rockot launch vehicle.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Aug 31, 03:31	7330	0.0009	945	959	104.10	99.27	316	06:01
2019 Sep 20, 12:36	7321	0.0001	943	943	103.90	99.27	111	06:01

Briz-KM rocket stage 2019-057B 44518					in space
Launched Cosmos 2540
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 30, 19:18	7188	0.0202	665	955	101.08	99.23	257

2019-058 Kuaizhou 1A Jiuquan Space Centre						2019 Aug 30, 23:41
Xiaoxiang-1 07 2019-058A 44519					in space
6U Cubesat fromTianyi Research Institute - testbed for technology involved in air traffic control from orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 31, 21:42	6979	0.0012	593	609	96.70	97.79	287

Taizhi 1 (KX-09) 2019-058B 44520					in space
Small satellite from the Innovation Academy for Microsatellites of the Chinese Academy of Sciences, conducting microgravity research.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 31, 21:41	6978	0.0011	592	607	96.68	97.79	291

Kuaizhou-1A upper stage 2019-058C 44521					in space
Launched Xiaoxiang-1 07 and KX-09.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Aug 31, 17:08	6898	0.0244	351	688	95.02	97.80	41

2019-059 CZ 4B Taiyuan Space Centre						2019 Sep 12, 03:26
Ziyuan-1 02D 2019-059A 44528					in space
Remote sensing satellite in sun-synchronous orbit. Equipped with a full-color high-resolution multi-spectral camera and a panchromatic camera. Its main tasks include production of images at 1:50,000 scale for use in land resource surveys to monitor disaster prevention measures, disaster mitigation, agriculture, forestry, water conservancy and the environment.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Sep 12, 20:07	7121	0.0012	735	752	99.68	98.58	264	10:30
2019 Sep 13, 17:39	7124	0.0009	739	752	99.73	98.58	267	10:30
2019 Sep 15, 05:47	7146	0.0008	762	774	100.19	98.58	162	10:30
2019 Sep 16, 16:54	7152	0.0001	773	775	100.33	98.58	111	10:30

Ice Pathfinder (BNU-1) 2019-059B 44529					in space
Small satellite mainly tasked with observing the environmental changes of the Antarctic and Arctic. Carries a multispectral camera; a high-resolution visible-light camera; and an Automatic Identification System AIS) receiver for relaying messages from ships at sea.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 13, 03:48	7120	0.0012	733	750	99.65	98.58	269

Jinniuzuo 1 (Taurus 1) 2019-059C 44530					in space
3U Cubesat from Aerospace System Engineering Research Institute of Shanghai for youth education and amateur radio. Carries an amateur radio payload and is equipped with an experimental solar sail to be deployed later in the mission to accelerate orbit decay.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 13, 12:07	7119	0.0013	732	751	99.64	98.59	271

CZ-4B rocket stage 2019-059D 44531					in space
Launched Ziyun-1 2D and others.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 13, 12:45	6974	0.0204	453	738	96.60	98.68	22

2019-060 CZ 11 Jiuquan Space Centre						2019 Sep 19, 06:42
Zhuhai-1 OVS-03 2019-060A 44534					in space
Commercial Chinese Earth observation satellite using high definition video. Data and imagery will be used to study vegetation, water and crops. Catalogue number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Sep 20, 06:05	6882	0.0013	495	513	94.69	97.40	277	13:00
2019 Oct 20, 04:22	6891	0.0015	502	523	94.88	97.40	197	12:59

Zhuhai-1 OHS-05 2019-060C 44536					in space
Commercial Chinese Earth observation satellite equipped with high definition, multispectral cameras. Data and imagery will be used to study vegetation, water and crops. Catalogue number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Sep 20, 06:05	6882	0.0012	495	512	94.69	97.40	280	13:00
2019 Oct 20, 10:26	6891	0.0011	505	520	94.88	97.41	193	12:59

Zhuhai-1 OHS-06 2019-060D 44537					in space
Commercial Chinese Earth observation satellite equipped with high definition, multispectral cameras. Data and imagery will be used to study vegetation, water and crops. Catalogue number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Sep 20, 06:05	6881	0.0013	494	511	94.67	97.40	283	13:00
2019 Oct 20, 10:02	6891	0.0010	506	520	94.88	97.40	212	12:59

Zhuhai-1 OHS-07 2019-060E 44538					in space
Commercial Chinese Earth observation satellite equipped with high definition, multispectral cameras. Data and imagery will be used to study vegetation, water and crops. Catalogue number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Sep 20, 06:04	6881	0.0014	493	512	94.67	97.40	282	13:00
2019 Oct 20, 09:55	6891	0.0010	506	519	94.88	97.40	197	12:59

Zhuhai-1 OHS-08 2019-060F 44539					in space
Commercial Chinese Earth observation satellite equipped with high definition, multispectral cameras. Data and imagery will be used to study vegetation, water and crops. Catalogue number and designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Sep 20, 13:41	6880	0.0015	492	512	94.65	97.40	286	13:00
2019 Oct 20, 01:50	6891	0.0008	507	518	94.88	97.41	219	12:59

CZ 11 upper stage 2019-060B 44535					Re-entered - 2019 Sep 19 Life <1 day
Launched cluster of Zuhai-1 satellites. Orbit was lowered soon after releasing the satellites in order to precipitate re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 19, 08:03	6702	0.0345	93	555	91.02	97.37	311
2019 Sep 19, 15:37	6606	0.0191	102	353	89.05	97.38	310

2019-061 CZ 3B + YZ-1 Xichang Space Centre						2019 Sep 22, 21:10
Beidou-3 M-23 2019-061A 44542					in space
Phase 2 operational satellite in MEO for China's navigation satellite system. Launch was brought forward by 24 hrs to avoid forecast bad weather at the launch site.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 24, 18:57	28248	0.0115	21546	22194	787.47	55.03	177
2019 Oct 01, 20:30	28205	0.0100	21547	22108	785.71	55.02	176
2019 Oct 26, 10:46	27909	0.0008	21508	21554	773.35	55.01	312

Beidou-3 M-24 2019-061B 44543					in space
Phase 2 operational satellite in MEO for China's navigation satellite system. Launch was brought forward by 24 hrs to avoid forecast bad weather at the launch site.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 24, 18:53	28242	0.0116	21535	22192	787.22	55.02	177
2019 Sep 28, 18:54	28154	0.0085	21535	22016	783.54	55.02	178
2019 Oct 04, 10:38	27906	0.0007	21507	21549	773.23	55.01	288

YZ-1 rocket stage 2019-061C 44544					in space
Launched pair of Beidou-3 satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 23, 14:12	28501	0.0032	22033	22213	798.08	55.14	234

CZ 3B rocket stage 2019-061D 44545					in space
Launched pair of Beidou-3 satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 23, 22:23	15765	0.5825	204	18569	328.32	55.02	171

2019-062 H-IIB (F-8) Tanegashima Space Centre						2019 Sep 24, 16:05
Kounotori 8 (HTV-8) 2019-062A 44546					Re-entered - 2019 Nov 3 Life 40 days
Carrying supplies and equipment to ISS. Precise launch time 16:05:05 UTC. Separated from launch vehicle at 16:20:07 UTC. Captured with ISS RMS Sep 28 at 11:13 UTC and docked with the downward-facing port of the ISS Harmony module at 15:08 UTC. Postponed from Sep 10 after a fire broke out on the launch pad. Undocked from Harmony Nov 1 at 1345 UTC by ISS RMS under ground control. Released into independent orbit at 17:21 UTC. Final retro-fire Nov 3 at 01:41 led to destructive re-entry at about 02:09 UTC. Any surviving fragments impacted the southern Pacific Ocean some 4500 km east of New Zealand at around 02:30 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 24, 18:55	6620	0.0112	167	316	89.33	51.67	321
2019 Sep 24, 20:25	6623	0.0085	188	301	89.40	51.66	313
2019 Sep 25, 19:12	6736	0.0010	351	365	91.70	51.66	278
2019 Sep 27, 18:42	6754	0.0016	365	386	92.06	51.65	191
2019 Sep 28, 03:52	6782	0.0006	400	408	92.65	51.64	88
2019 Sep 28, 07:16	6793	0.0006	411	420	92.87	51.64	94
2019 Sep 28, 12:46	6795	0.0007	411	421	92.90	51.64	93
2019 Oct 31, 13:30	6794	0.0006	412	420	92.89	51.65	210
2019 Nov 01, 20:20	6788	0.0006	406	414	92.76	51.65	215
2019 Nov 02, 22:52	6693	0.0087	256	373	90.82	51.97	286
2019 Nov 03, 00:26	6650	0.0191	145	399	89.94	51.64	296

H-IIB upper stage					Re-entered - 2019 Sep 24 Life <1 day
Launched Kounotori 8. De-orbited shortly after releasing its payload so not catalogued.
Not Catalogued - orbit parameters unavailable

2019-063 CZ 2D Jiuquan Space Centre						2019 Sep 25, 00:54
Yunhai-1 2 2019-063A 44547					in space
Meteorological satellite developed by the Shanghai Academy of Spaceflight Technology (SAST) to be used for observation of atmospheric, marine and space environments, disaster prevention and scientific experiments.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Sep 25, 05:57	7152	0.0009	767	780	100.32	98.58	269	07:10
2019 Sep 30, 10:57	7161	0.0001	782	784	100.52	98.59	278	07:10

CZ 3B upper stage 2019-063B 44548					in space
Launched Yunhai 1 2.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 26, 08:03	7139	0.0008	755	767	100.05	98.15	16

2019-064 Soyuz-FG Baikonur Cosmodrome						2019 Sep 25, 13:57
Soyuz MS-15 (Soyuz 11F732A48 № 745) 2019-064A 44550					Re-entered - 2020 Apr 17 Life 205 days Returned to Earth
Carrying crew to ISS - Oleg Skripochka (Roscosmos), Jessica Meir (NASA), Hazza Al Mansouri (UAE spaceflight participant). Precise launch time 13:57:43 UTC. Docked with rear port of Zvezda at 19:42 UTC. Undocked 2020 Apr 17 at 01:53 UTC carrying Skripochka, Meir and Andrew Morgan (NASA). Retrofire at 04:22 UTC led to landing at 05:16:43 UTC, 147 km south east of Dzhezkazgan, Kazakhstan.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 25, 14:26	6583	0.0015	195	215	88.59	51.64	68
2019 Sep 25, 17:01	6736	0.0028	339	377	91.70	51.66	206
2019 Sep 25, 17:01	6795	0.0007	411	421	92.90	51.64	84
2020 Apr 16, 12:06	6799	0.0004	418	423	92.98	51.64	121

Soyuz upper stage 2019-064B 44551					Re-entered - 2019 Sep 28 Life 3 days
Launched Soyuz MS-15.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 25, 19:40	6578	0.0008	195	205	88.49	51.65	40

2019-065 Soyuz-2 1B + Fregat Plesetsk Cosmodrome						2019 Sep 26, 08:46
Cosmos 2541 (EKS 3/Tundra 3) 2019-065A 44552					in space
EKS missile early warning satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Sep 26, 15:51	26469	0.6969	1646	38537	714.29	63.83	270
2019 Oct 08, 07:33	26551	0.6983	1633	38712	717.59	63.84	270

Fregat-M stage 2019-065B 44553					in space
Launched Cosmos 2541.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 02, 08:13	26475	0.6968	1648	38545	714.51	63.82	270

2019-066 CZ 4C Taiyuan Space Centre						2019 Oct 4, 18:51
Gaofen 10 2019-066A 44622					in space
Remote sensing satellite to be used for land use surveys, urban planning, road network design, crop estimation and disaster prevention/mitigation, part of a remote sensing programme based on LEO and GEO satellites. Replaces the original Gaofen 10 that was lost in a launch failure 2016 Aug 31. An unspecified issue on Oct 2 caused 24 hr launch postponement from Oct 3.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Oct 05, 04:01	6995	0.0007	612	622	97.04	97.78	252	01:59
2019 Oct 11, 23:54	7003	0.0004	622	628	97.21	97.77	16	01:59
2019 Oct 13, 03:03	7006	0.0000	628	628	97.27	97.78	262	01:59

CZ 4C upper stage 2019-066B 44623					in space
Launched Gaofen 10.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 04, 21:30	6902	0.0129	434	613	95.10	97.75	39

2019-067 Proton-M + Briz-M Baikonur Cosmodrome						2019 Oct 9, 10:17
Eutelsat 5 West B 2019-067A 44624					in space
Comsat to join Eutelsat 5 West A and eventually take over its functions. Coverage is aimed at France, Italy and Algeria. Satellite includes GEO 3, an EGNOS (European Geostationary Navigation Overlay Service) to improve the precision of ESA's Galileo navigation system for users needing very accurate position information. Precise launch time 10:17:56 UTC. Released from the launch vehicle Oct 10 at 01:53 UTC. Oct 24, Eutelsat revealed an unspecified problem with one of the solar arrays (probably not having deployed fully, if at all). 2020 Jan 17, Eutelsat confirmed the south solar array did not deploy and the satellite is working at 45% capacity. Expected location - 5° west.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Oct 10, 15:21	44913	0.5910	11989	65080	1578.75	13.36	179
2019 Oct 14, 10:25	53994	0.3193	30374	64857	2081.00	3.36	179
2019 Oct 18, 15:00	56748	0.2552	35888	64852	2242.28	1.99	179
2019 Oct 19, 23:13	47728	0.1151	35855	46846	1729.52	0.97	178
2019 Oct 21, 13:56	43726	0.0345	35842	38855	1516.61	0.28	174
2019 Oct 22, 09:42	42234	0.0005	35834	35878	1439.63	0.03	102	4° east
2019 Oct 28, 14:44	42164	0.0001	35781	35792	1436.07	0.01	232	2° east
2020 Jan 10, 23:07	42165	0.0002	35779	35794	1436.11	0.06	52	2° east
2020 Jan 13, 15:20	42271	0.0002	35885	35901	1441.54	0.05	333	2° west
2020 Jan 17, 07:40	42167	0.0002	35782	35797	1436.24	0.05	111	5° west

MEV-1 (Mission Extension Vehicle 1) 2019-067B 44625					in space
Northrop Grumman spacecraft - launched to rendezvous and attach itself to the Intelsat 901 GEO comsat (28624/2001-024A) then take over its pointing and station-keeping functions in order to extend its on-orbit life by five years. May then move to another satellite. Precise launch time 10:17:56 UTC. Released from the launch vehicle Oct 10 at 02:11 UTC into super-synchronous orbit then pushed towards Intelsat rendezvous by onboard electric thruster system, arriving 2020 Jan 31. Intelsat 901 had departed its station at 27°.5 east 2019 Dec 11 and moved to GEO graveyard orbit. MEV-1 then docked with Intelsat 901 on 2020 Feb 25 at 07:15 UTC so all subsequent listed orbits are for the combined objects. Arrived at Intelsat 901 new location of 27°.5 west 2020 Mar 29.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Oct 10, 15:18	44842	0.5906	11979	64948	1575.01	13.39	179
2019 Oct 14, 11:02	46021	0.5479	14429	64857	1637.57	9.81	179
2019 Nov 22, 20:00	45425	0.3862	21505	56589	1605.84	5.20	188
2019 Nov 26, 11:14	45439	0.3863	21510	56613	1606.60	5.21	189
2019 Dec 29, 03:25	44186	0.2172	28209	47407	1540.59	2.74	207
2020 Jan 03, 05:00	44190	0.2173	28212	47413	1540.81	2.75	207
2020 Jan 23, 03:30	42982	0.0542	34272	38935	1478.03	1.63	251
2020 Jan 29, 00:22	42667	0.0208	35401	37175	1461.81	1.57	266	118° west
2020 Jan 31, 17:34	42485	0.0035	35956	36258	1452.50	1.56	294	132° west
2020 Feb 25, 13:28	42467	0.0002	36081	36098	1451.59	1.64	351	132° east
2020 Mar 03, 13:33	42616	0.0002	36228	36247	1459.22	1.42	340	97° east
2020 Mar 12, 14:01	42616	0.0003	36227	36250	1459.22	0.86	358	45° east
2020 Mar 17, 16:11	42619	0.0003	36227	36255	1459.38	0.56	353	16° east
2020 Mar 22, 07:05	42622	0.0003	36229	36258	1459.50	0.22	342	11° west
2020 Mar 26, 00:00	42272	0.0011	35847	35942	1441.60	0.32	7	24° west
2020 Mar 26, 04:48	42230	0.0001	35848	35857	1439.45	0.17	55	25° west
2020 Mar 29, 07:39	42231	0.0001	35849	35857	1439.49	0.06	43	27° west
2020 Mar 30, 11:16	42165	0.0001	35781	35793	1436.11	0.06	113	27° west

Briz-M rocket stage 2019-067C 44626					in space
Launched Eutelsat 5 West B and MEV-1. Performed a separation manoeuvre after releasing MEV-1. Orbits shown are estimates based on data from Khrunichev, the launch vehicle operator, covering the stages of flight leading up to satellite separation. Catalogue Number and Designation to be confirmed. Space-Track orbit data awaited.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 09, 10:33	6567	0.0012	181	197	88.27	51.55	80
2019 Oct 09, 12:28	9531	0.2995	298	6007	154.33	50.40	179
2019 Oct 09, 15:02	39119	0.8251	465	65016	1283.32	50.10	180
2019 Oct 10, 01:53	45073	0.5831	12412	64977	1587.18	13.40	180
2019 Oct 10, 04:12	43935	0.6119	10675	64438	1527.45	13.30	180

Briz-M APT 2019-067D 44627					in space
Discarded propellant tank from Briz-M rocket stage.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 09, 18:03	16228	0.5846	363	19336	342.88	50.35	173

2019-068 Pegasus XL Lockheed L-1011 over Atlantic Ocean near Cape Canaveral AFS						2019 Oct 11, 01:59
ICON (Ionospheric Connection Explorer) 2019-068A 44628					in space
NASA satellite to study the influences of terrestrial weather and space weather on the ionosphere. The L-1011 took off from Cape Canaveral AIr Force Station at 00:31 UTC and climbed to about 12,500 metres. The Pegaus rocket was released thirty four minutes into a ninety minute launch window that opened at 01:25 UTC. The originally planned release at 01:30 UTC was abandoned because of communications dificulties between the aircraft and the ground. Delayed one day from Oct 10 due to weather.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 14, 22:43	6971	0.0019	580	606	96.54	26.99	169

Pegasus upper stage. 2019-068B 44629					in space
Launched ICON.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 14, 22:40	6968	0.0016	579	602	96.49	27.00	166

2019-069 Electron Rocket Lab LC-1, New Zealand						2019 Oct 17, 01:22
Palisade 2019-069A 44634					in space
Imaging satellite owned by Aquila Systems, built to test systems for upcoming satellites based on its 16U (4x4, non-standard Cubesat) Corvus platform. Released from Electron kick stage at 02:33 UTC. Launch delayed from Oct 14 due to thunderstorms in the launch area.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 17, 20:21	7594	0.0011	1208	1224	109.77	87.90	117

Electron upper stage 2019-069B 44635					in space
Launched Palisade satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 17, 18:44	7136	0.0629	309	1206	99.98	87.89	272

Electron kick stage 2019-069C 44636					in space
Launched Palisade satellite. Performed a perigee-lowering engine firing after releasing the satellite into circular orbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 18, 13:50	7229	0.0503	487	1215	101.95	87.90	24

2019-070 CZ 3B Xichang Space Centre						2019 Oct 17, 15:21
TJS 4 (Communications Technology Experiment Satellite 4) 2019-070A 44637					in space
Described as a technology test satellite, TJS 4 is probably military in nature and intended for signals intelligence gathering (SIGINT).
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Oct 18, 03:45	24387	0.7303	200	35818	631.68	27.03	180
2019 Oct 29, 15:28	42166	0.0003	35775	35800	1436.14	0.09	276	84° east
2019 Nov 09, 02:47	42164	0.0003	35771	35800	1436.03	0.06	280	84° east

CZ 3B upper stage 2019-070B 44638					in space
Launched TJS 4.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Oct 18, 03:41	23963	0.7256	197	34973	615.27	27.01	179

2019-071 Antares 230 Wallops Flight Facility						2019 Nov 2, 13:59
SS Alan Bean (Cygnus NG-12) 2019-071A 44701					Re-entered - 2020 Mar 17 Life 136 days
Northrop Grumman vehicle carrying supplies to ISS under CRS-2 contract with NASA. Precise launch time 13:59:47 UTC at the beginning of approximately five minute window. Separated from launch vehicle 14:07:36 UTC. Arrived ISS Nov 4 and captured by ISS RMS at 09:10 UTC under control of crew. Docked with downward-facing port of Unity module using RMS under control of ground-based engineers at 11:21 UTC. Undocked 2020 Jan 31 then released from RMS at 13:36 UTC the same day. Whilst in post-undocking free flight, Cygnus released a number of Cubesats and hosted a payload for the US company, Lynk, for experimentation in using space based-mobile phone cells. Planned re-entry 2020 Mar 2 was delayed in order to extend the Lynk tests. Retro fire Mar 17 around 23:00 UTC led to re-entry above the southern Pacific Ocean around 23:40 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 02, 15:36	6637	0.0021	244	273	89.68	51.62	139
2019 Nov 03, 03:23	6726	0.0101	280	416	91.50	51.64	239
2019 Nov 03, 11:09	6775	0.0028	378	416	92.50	51.64	243
2019 Nov 04, 05:34	6790	0.0006	408	416	92.81	51.65	214
2020 Jan 31, 18:10	6799	0.0004	418	424	92.99	51.64	217
2020 Feb 01, 11:53	6843	0.0009	458	471	93.89	51.65	271
2020 Mar 17, 13:36	6841	0.0012	454	471	93.84	51.62	52

Orbital Factory 2 2019-071C 45113					in space
1U Cubesat from the University of Texas at El Paso (UTEP). It carries a 3D printer to demostrate the concept of conducting repairs on a solar cell. Released from Cygnus NG-12 Slingshot deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 04, 00:09	6846	0.0013	459	476	93.94	51.64	295

Aerocube 14A 2019-071D 45114					in space
3U Cubesat, one of a pair, equipped to demonstrate a new star-tracker technology, test a selection of new materials and test a new solar cell. Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 01, 19:30	6846	0.0011	460	475	93.94	51.64	278

SwampSat II 2019-071E 45115					in space
3U Cubesat from the University of Florida to measure VLF (Very Low Frequency) waves in the ionosphere. It is equipped with a 4m x 4m deployable aerial. Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 04, 07:59	6846	0.0013	459	476	93.95	51.64	297

Aerocube 14B 2019-071F 45116					in space
3U Cubesat, one of a pair, equipped to demonstrate a new star-tracker technology, test a selection of new materials and test a new solar cell. Released from Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 02, 10:36	6845	0.0011	460	475	93.94	51.64	293

Aerocube 15B 2019-071G 45117					in space
3U Cubesat one of a pair from Aerospace Corporation to test a low cost optical imager. Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 07, 20:27	6845	0.0011	459	474	93.93	51.64	308

Aerocube 15A 2019-071H 45118					in space
3U Cubesat one of a pair from Aerospace Corporation to test a low cost optical imager. Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 10, 20:24	6845	0.0011	459	474	93.92	51.64	318

Very Low Frequency Propagation Mapper 2019-071K 45120					in space
6U Cubesat from USAF Research Lab. Will study the progagtion of VLF radio signals within the magnetospher, using transmissions from the DSX satelli already in orbit (44344/2019-036F). Released from Cygnus NG-12 Slingshot deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 10, 20:24	6844	0.0011	458	474	93.92	51.64	317

CIRiS (Compact Infrared Radiometer in Space) 2019-071L 45121					in space
6U Cubesat from Utah State University to collect, process and calibrate infrared images to measure the temparuture of the Earth’s surface below. Built by Ball Aerospace. Released from Cygnus NG-12 Slingshot Deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 10, 20:23	6844	0.0011	458	474	93.92	51.64	316

ORCA 8 2019-071R 45126					in space
6U Cubesat from US Defense Advanced Research Projects Agency (DARPA). Onboard equipment is From Systems and Technology Research, a US company that specialises in sensors relating to image processing clandestine communications and SIGINT (among others). Released from Cygnus NG-12 Slingshot deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Feb 10, 20:23	6844	0.0010	459	473	93.92	51.64	289

EdgeCube 2019-071xx					in space
1U Cubesat from Sonoma State University of California in partnership with Morehead State University in Kentucky. It will study chlorophyl by measuring seasonal and other changes in light reflection from leaves. Released from Cygnus NG-12 Slingshot deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
estimated orbit	6846	0.0011	460	475	93.94	51.64	278

HuskySat 1 2019-071xx					in space
3U Cubesat from the University of Washington to demonstrate plasma propulsion and high gain telemetry system for potential use in cubesats operating as far away as the Moon. Released from Cygnus NG-12 Nanoracks deployer 2020 Jan 31, around 21:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
estimated orbit	6846	0.0012	459	476	93.95	51.64	282

MiniCarb 2019-071xx					in space
6U Cubesat developed by NASA, the Lawrence LIvermore National Laboratory and the USAF to detect and measure the amounts of greenhouse gases, such as methane and carbon dioxide, in the Earth's atmosphere. Released from Cygnus NG-12 Slingshot deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
estimated orbit	6844	0.0011	458	474	93.92	51.64	317

Antares upper stage 2019-071B 44702					Re-entered - 2019 Nov 7 Life 5 days
Launched SS Alan Bean.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 02, 15:36	6600	0.0053	187	257	88.94	51.63	125

2019-072 CZ 4B Taiyuan Space Centre						2019 Nov 3, 03:22
Gaofen 7 2019-072A 44703					in space
Civilian high resolution stereoscopic Earth imaging satellite for mapping.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Nov 04, 23:00	6875	0.0013	488	506	94.55	97.49	266	10:31
2019 Nov 30, 19:25	6880	0.0011	495	510	94.66	97.49	155	10:32

SRSS 1 (Sudanese Remote Sensing Satellite) 2019-072B 44704					in space
Small satellite developed for the Sudanese government by the Shenzhen Aerospace Oriental Red Sea Satellite Co. Designed for both civil and military remote sensing mainly over Sudan.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 05, 21:35	6873	0.0013	486	504	94.52	97.50	268

Huangpu 1 2019-072C 44705					in space
Small developmental/test satellite for remote sensing built by the Shanghai Aerospace Technology Research Institute.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 04, 11:00	6873	0.0014	485	505	94.51	97.48	277

Xiaoxiang-1 08 2019-072D 44706					in space
6U Cubesat from Tianyi Research Institute - testbed for multispectral remote sensing imaging system for agricultural crop surveys. Also carries a laser communication system and a cold gas thruster to speed up orbital decay at end of life.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 04, 11:00	6873	0.0016	484	506	94.52	97.49	268

CZ-4B upper stage 2019-072E 44707					Re-entered - 2020 Apr 8 Life 157 days
Launched Gaofen 7. Performed an orbit-lowering engine firing after releasing its satellites in order to accelerate re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 03, 09:00	6738	0.0196	228	492	91.75	97.59	28

2019-073 CZ 3B Xichang Space Centre						2019 Nov 4, 17:43
Beidou-3 IGEO-3 2019-073A 44709					in space
Phase 2 operational satellite in China's navigation satellite system. It also provides time and messaging services for the Asia-Pacific region from inclined geosynchronous orbit. Probably moved into geosynchronous drift orbit some time on Nov 5 and arrived on station shortly after. Launch completes the IGEO part of the Beidou-3 constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Nov 04, 23:24	24384	0.7309	184	35828	631.57	28.51	180
2019 Nov 22, 20:40	42159	0.0025	35675	35888	1435.81	58.70	184	106° east

CZ 3B upper stage 2019-073B 44710					in space
Launched Beidou-3 IGEO-3.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 04, 20:52	23652	0.7239	152	34396	603.33	28.50	179

2019-074 Falcon 9 Block 5 Cape Canaveral						2019 Nov 11, 14:56
Starlink-1007 2019-074A 44713					in space
One member of a simultaneously-launched cluster of sixty LEO Broadband communications satellites from SpaceX aimed ultimately at 550 km altitude. Separated from the launch vehicle around 15:57 UTC. All satellites were injected initially into similar orbits at 300 km altitude.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 14, 22:00	6678	0.0001	299	300	90.51	53.01	326
2019 Nov 28, 12:00	6728	0.0001	349	351	91.53	53.01	46
2020 Jun 20, 04:00	6928	0.0001	549	550	95.64	53.00	105

Falcon 9 upper stage					Re-entered - 2019 Nov 11 Life <1 day
Launched cluster of Starlink satellites. Caused to re-enter about one hour after lift-off. Any surviving fragments from its destructive re-entry impacted the Southern Ocean. Not catalogued.
Not Catalogued - orbit parameters unavailable

2019-075 Kuaizhou-1A Jiuquan Space Centre						2019 Nov 13, 03:40
Jilin-1 High Resolution 02A 2019-075A 44777					in space
Chinese high resolution, multi-spectral imaging satellite. Launch postponed from Oct 27 (weather) and Oct 29 (problem with launch vehicle guidance system).
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Nov 15, 04:43	6917	0.0011	532	546	95.42	97.54	255	10:00

Kuaizhou-1A upper stage 2019-075B 44778					Re-entered - 2019 Nov 20 Life 7 days
Launched Jilin-1 02A. Performed a retro-fire after releasing the satellite in order to speed up re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 13, 06:23	6765	0.0362	142	631	92.29	97.50	25

2019-076 CZ 6 Taiyuan Space Centre						2019 Nov 13, 06:35
Ningxia-1 01 (Zhongzi 1) 2019-076A 44779					in space
One of a cluster of five similar satellites. Described as a "commercial electromagnetic signal monitoring satellite", it is probably designed to monitor radio traffic from ships and aircraft over uninhabited or offshore areas. Built by the Ningxia Jingui Information Technology Co.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 14, 11:13	7271	0.0008	887	899	102.84	45.00	257

Ningxia-1 02 (Zhongzi 2) 2019-076B 44780					in space
One of a cluster of five similar satellites. Described as a "commercial electromagnetic signal monitoring satellite", it is probably designed to monitor radio traffic from ships and aircraft over uninhabited or offshore areas. Built by the Ningxia Jingui Information Technology Co.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 13, 23:13	7271	0.0008	887	899	102.84	45.01	254
2019 Nov 20, 21:19	7270	0.0009	885	899	102.81	45.01	285

Ningxia-1 03 (Zhongzi 3) 2019-076C 44781					in space
One of a cluster of five similar satellites. Described as a "commercial electromagnetic signal monitoring satellite", it is probably designed to monitor radio traffic from ships and aircraft over uninhabited or offshore areas. Built by the Ningxia Jingui Information Technology Co.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 13, 23:13	7270	0.0009	886	899	102.82	45.00	263
2019 Nov 19, 00:46	7269	0.0011	882	898	102.79	45.00	274

Ningxia-1 04 (Zhongzi 4) 2019-076D 44782					in space
One of a cluster of five similar satellites. Described as a "commercial electromagnetic signal monitoring satellite", it is probably designed to monitor radio traffic from ships and aircraft over uninhabited or offshore areas. Built by the Ningxia Jingui Information Technology Co.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 13, 11:48	7270	0.0010	885	899	102.81	45.01	272
2019 Nov 20, 04:08	7267	0.0012	880	898	102.76	45.01	283

Ningxia-1 05 (Zhongzi 5) 2019-076E 44783					in space
One of a cluster of five similar satellites. Described as a "commercial electromagnetic signal monitoring satellite", it is probably designed to monitor radio traffic from ships and aircraft over uninhabited or offshore areas. Built by the Ningxia Jingui Information Technology Co.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 13, 21:30	7269	0.0009	884	898	102.79	45.00	277
2019 Nov 17, 21:20	7266	0.0012	879	896	102.73	45.01	292

CZ 6 upper stage 2019-076F 44784					in space
Launched group of five Ningxia-1 satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 14, 12:34	7212	0.0089	770	898	101.59	45.01	8

2019-077 Kuaizhou 1A Taiyuan Space Centre						2019 Nov 17, 10:00
KL-alpha A 2019-077A 44785					in space
One of a pair of proof-of-concept satellites for a multi-media communications system. Built by the Institute of Microsatellite Innovation of the Chinese Academy of Sciences to be operated by a German company, KLEO Connect, that has the contract to provide demonstrator satellites for the proposed "eightyLEO" constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 17, 18:11	7429	0.0009	1044	1058	106.21	88.91	275

KL-alpha B 2019-077B 44786					in space
One of a pair of proof-of-concept satellites for a multi-media communications system. Built by the Institute of Microsatellite Innovation of the Chinese Academy of Sciences to be operated by a German company, KLEO Connect, that has the contract to provide demonstrator satellites for the proposed "eightyLEO" constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 17, 18:27	7617	0.0254	1045	1432	110.26	88.91	309

Kuaizhou-1A upper stage 2019-077C 44787					in space
Launched KL-alpha pair. Performed retro-fire soon after releasing satellites in order to hasten re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 17, 21:01	7097	0.0546	331	1106	99.16	88.88	185

2019-I12 JEM Small Satellite Orbital Deployer International Space Station						2019 Nov 20, 09:50
RwaSat 1998-067QV 44790					in space
3U Cubesat from Rwanda, built with assistance from Japan. It carries a store and forward messaging system and Earth observation cameras. Release time shown is as planned - actual time not confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 21, 19:53	6793	0.0009	409	420	92.86	51.64	327

2019-I13 JEM Small Satellite Orbital Deployer International Space Station						2019 Nov 20, 10:09
AqT-D (Aqua Thruster - Demonstrator) 1998-067QW 44791					in space
3U Cubesat from the University of Tokyo to demonstrate water as a propellant for satellite thrusters. Release time shown is as planned - actual time not known.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 21, 07:50	6793	0.0003	413	416	92.86	51.64	310

2019-I14 JEM Small Satellite Orbital Deployer International Space Station						2019 Nov 20, 10:10
NARSSCube 1 1998-067QX 44792					in space
1U Cubesat from Egypt's National Authority for Remote Sensing and equipped with an Earth observation camera. Release time shown is as planned - actual time not confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 21, 10:55	6793	0.0005	412	419	92.87	51.64	327

2019-078 CZ 3B + YZ-1 Xichang Space Centre						2019 Nov 23, 00:55
Beidou-3 M-21 2019-078A 44793					in space
Phase 2 operational satellite in MEO for China's navigation satellite system.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 29, 05:24	28247	0.0115	21542	22194	787.42	54.99	178
2019 Dec 14, 01:28	28108	0.0066	21545	21916	781.65	55.00	180
2019 Dec 20, 13:59	27907	0.0006	21512	21545	773.26	55.01	332

Beidou-3 M-22 2019-078B 44794					in space
Phase 2 operational satellite in MEO for China's navigation satellite system.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 25, 03:21	28243	0.0116	21537	22192	787.26	54.99	178
2019 Dec 30, 06:01	27906	0.0005	21514	21542	773.22	55.00	323

YZ-1 rocket stage 2019-078C 44795					in space
Launched Beidou-3 M-21 and Beidou-3 M-22.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 23, 07:12	28737	0.0058	22193	22526	808.03	55.15	359

CZ 3B upper stage 2019-078D 44796					in space
Launched Beidou-3 M-21 and Beidou-3 M-22.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 23, 04:16	15744	0.5819	204	18527	327.65	54.96	171

2019-079 Soyuz-2 1V Plesetsk Cosmodrome						2019 Nov 25, 17:52
Cosmos 2542 2019-079A 44797					in space
Military satellite with sensors that allow it to observe other satellites in orbit. It also carries an Earth imaging system. Orbit is very close to, and co-planar with, that of USA 245 (39232/2013-043A), a KH-11 reconsat.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Nov 26, 12:54	6991	0.0350	368	858	96.96	97.90	319	09:40

Cosmos 2543 2019-079D 44835					in space
Small satellite detached from Cosmos 2542 on Dec 6 probably sometime between 04:00 UTC and 10:00 UTC. Purpose possibly connected with the 'observing other satellites' capability mentioned in the launch announcement for Cosmos 2542.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 06, 13:49	6991	0.0351	368	858	96.95	97.90	286	09:40
2019 Dec 09, 16:11	6993	0.0347	372	858	96.99	97.90	276	09:40
2019 Dec 14, 15:58	7034	0.0287	454	858	97.86	97.90	260	09:40
2019 Dec 16, 17:02	7103	0.0189	590	859	99.29	97.90	253	09:40
2020 Jul 16, 18:52	6989	0.0010	604	618	96.91	97.87	141	09:07

Cosmos 2547? 2019-079E 45915					in space
Test of kinetic energy satellite interceptor using Cosmos 2535 (44421/2019-035A) as a target. Released from Cosmos 2543 (44835/2019-079D) 2020 Jul 17 and passed close to Cosmos 2535. Possibly aimed for a near miss in order to avoid a debris-shedding event.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2020 Jul 16, 19:07	7022	0.0198	505	784	97.61	97.87	183

Volga rocket stage 2019-079B 44798					Re-entered - 2019 Nov 26 Life 1 day
Launched Cosmos 2542. Caused to re-enter over the southern Pacific Ocean Nov 26 with retro-fire at approx 05:30 UTC and entry into the atmosphere at about 06:10 UTC on a track heading northward from Antarctica.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 26, 04:49	6992	0.0352	368	860	96.98	97.90	320

Soyuz upper stage 2019-079C 44799					Re-entered - 2020 Jul 18 Life 236 days
Launched Cosmos 2542.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 26, 05:50	6704	0.0056	289	364	91.06	97.91	67

2019-080 Ariane 5 ECA (VA-250) Centre Spatiale Guyanaise						2019 Nov 26, 21:23
TIBA 1 2019-080A 44800					in space
Egyptian government and military communications satellite. Separated from launch vehicle at 21:50 UTC. Launch postponed from Nov 22 by problem with ground equipment then delayed 14 mins by weather. Expected location - 35°.5 east.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Nov 27, 00:08	24392	0.7276	266	35763	631.88	5.00	178
2019 Dec 02, 03:09	36448	0.1556	24401	35740	1154.19	0.51	173
2019 Dec 07, 22:30	42154	0.0009	35737	35814	1435.54	0.07	254	36° east
2019 Dec 08, 04:19	42163	0.0003	35774	35795	1436.00	0.07	324	36° east

Inmarsat 5 F5 (GX-5) 2019-080B 44801					in space
High capacity comsat proving services to the Middle East, Europe and the Indian sub-continent. Fifth satellite in Intelsat's Global Express constellation. Separated from launch vehicle at 22:07 UTC. Launch postponed from Nov 22 by problem with ground equipment then delayed 14 mins by weather. Expected location - 11° east.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Nov 27, 13:40	24365	0.7277	256	35719	630.84	5.00	178
2019 Dec 03, 15:56	42059	0.0001	35677	35685	1430.70	0.08	128	80° east
2019 Dec 05, 22:36	42086	0.0004	35690	35725	1432.05	0.08	262	83° east
2019 Dec 08, 07:45	42156	0.0012	35728	35828	1435.66	0.07	104	84° east
2019 Dec 10, 16:54	42164	0.0000	35786	35786	1436.08	0.07	45	84° east

Ariane 5 upper stage 2019-080C 44802					in space
Launched TIBA 1 and Eutelsat 5 F5.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 26, 23:59	24256	0.7266	252	35503	626.59	5.06	179

2019-081 PSLV XL (C-47) Satish Dhawan Space Centre						2019 Nov 27, 03:58
Cartosat 3 2019-081A 44804					in space
Indian third generation high resolution imaging cartographic and remote sensing satellite. Separated from launch vehicle at 04:15 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Nov 27, 11:38	6888	0.0014	500	519	94.82	97.52	232	09:29

Meshbed 2019-081C 44806					in space
3U Cubesat from Analytical Space Inc, testing its FUSE experimental phased array communication antenna.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 28, 23:35	6887	0.0013	500	518	94.79	97.52	235

Flock 4P-1 2019-081L 44814					in space
3U Cubesat, part of Planet's Flock 4P cluster of second generation imaging satellites. The satellite is one of a cluster of twelve Flock 4P satellites carried on this launch. In order to avoid clutter the others are not listed separately. All are are in similar orbits.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 29, 12:13	6885	0.0013	498	516	94.77	97.52	215

PSLV upper stage 2019-081B 44805					in space
Launched Cartosat 3 and thirteen small satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 27, 06:53	6908	0.0046	498	561	95.23	97.51	239

2019-082 CZ 4C Taiyuan Space Centre						2019 Nov 27, 23:52
Gaofen 12 2019-082A 44819					in space
Earth observation using radar to support land surveys, crop management, urban and road network planning.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Nov 28, 04:09	6975	0.0004	594	599	96.62	97.93	252	07:00
2019 Nov 29, 13:10	6993	0.0002	613	616	96.99	97.93	172	07:00
2019 Nov 30, 13:16	7003	0.0004	623	628	97.21	97.94	349	07:00
2019 Dec 01, 19:29	7007	0.0001	628	630	97.28	97.93	74	07:00

CZ 4C upper stage 2019-082B 44820					in space
Launched Gaofen 12. Performed a separation manoeuvre and moved into a slightly lower orbit after satellite release.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Nov 28, 04:05	6884	0.0128	418	594	94.74	97.88	44

2019-083 Falcon 9 Block 5 Cape Canaveral						2019 Dec 5, 17:29
SpaceX Dragon CRS-19 2019-083A 44821					Re-entered - 2020 Jan 7 Life 33 days Returned to Earth
Supplies to ISS. Captured by ISS Remote Manipulator System under manual control Dec 8 at 10:05 UTC. Docked, using the RMS under ground control, with the downward-facing port of the Harmony node at 12:47 UTC. Undocked using RMS under ground control, 2020 - Jan 6 or Jan 7, released under ground control Jan 7, 10:05 UTC, two minutes later than scheduled. Retro fire Jan 7, approx14:47 UTC led to splashdown off California near 31° north, 121° west at 15:42 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 05, 23:30	6669	0.0130	204	378	90.34	51.65	49
2019 Dec 07, 04:37	6668	0.0134	201	379	90.32	51.65	54
2019 Dec 07, 21:17	6784	0.0013	397	415	92.68	51.64	13
2019 Dec 08, 14:18	6795	0.0007	411	422	92.90	51.64	12

Falcon 9 upper stage					Re-entered - 2019 Dec 5 Life <1 day
Launched Dragon CRS-19. Caused to re-enter shortly after releasing Dragon.
Not Catalogued - orbit parameters unavailable

2019-084 Electron Rocket Lab LC-1, New Zealand						2019 Dec 6, 08:18
ALE 2 (Astro Live Experiences 2) 2019-084A 44824					in space
Satellite aimed to create 400 artificial meteors in a selection of colours (white, green, pink and orange) partly as performance art. The satellite includes a propulsion system for maneuvers.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 11:02	6784	0.0013	397	415	92.69	97.01	307

NOOR 1A 2019-084D 44827					in space
Satellite from Stara Space to demonstrate LEO-to-LEO intersatellite link technology, including on-demand provision of communication links to ground stations.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 07, 04:56	6754	0.0041	348	403	92.06	97.00	254

NOOR 1B 2019-084E 44828					Re-entered - 2020 Apr 7 Life 123 days
Satellite from Stara Space to demonstrate LEO-to-LEO intersatellite link technology, including on-demand provision of communication links to ground stations.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 19:43	6753	0.0040	348	402	92.05	97.00	256

Fossasat 1 2019-084F 44829					in space
Small satellite developed by Spain's Fossa Systems - communications satellite that uses low power RF to provide internet connectivity.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 21:20	6753	0.0040	348	401	92.04	97.00	254

ATL 1 (Advanced Technology of Laser) 2019-084G 44830					in space
Small satellite from Advanced Technology of Laser from Hungary designed to test a new thermal isolation material in space, conduct a thermal insulator material experiment, and DVB-T band spectrum monitoring.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 21:20	6753	0.0041	347	402	92.04	97.01	255

TRSI Sat 2019-084H 44831					in space
Small satellite conducting tests on decoding weak signals and testing a very small satellite transmit/receive aerial. Catalogue Number and Designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 21:19	6753	0.0037	350	399	92.04	97.01	251

SMOG-P 2019-084J 44832					in space
Spectrum monitoring payload built by students at the Budapest University of Technology and Economics in Hungary. It features a radio spectrum analyzer to measure man-made electromagnetic pollution from space.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 21:19	6752	0.0039	348	401	92.03	97.00	253

Electron kick stage 2019-084B 44825					in space
Launched cluster of satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 16:39	6755	0.0051	342	412	92.09	97.00	257

Electron upper stage 2019-084C 44826					Re-entered - 2019 Dec 18 Life 12 days
Launched cluster of satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 10:52	6672	0.0172	180	409	90.40	97.01	225

2019-085 Soyuz-2 1A Baikonur Cosmodrome						2019 Dec 6, 09:34
Progress MS-13 (Progress 7K-TGM №443) 2019-085A 44833					Re-entered - 2020 Jul 8 Life 215 days
Supplies to ISS. Precise launch time 09:34:11 UTC. Docked automatically with Pirs module of ISS Dec 9 at 10:35:11 UTC, about 3 min earlier than scheduled.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 17:07	6697	0.0008	313	324	90.90	51.63	25
2019 Dec 06, 21:23	6699	0.0012	312	329	90.94	51.64	17
2019 Dec 08, 12:45	6704	0.0020	312	339	91.04	51.65	21
2019 Dec 09, 13:27	6795	0.0007	411	421	92.90	51.64	17

Soyuz upper stage 2019-085B 44834					Re-entered - 2019 Dec 10 Life 4 days
Launched Progress MS-13.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 06, 18:41	6581	0.0024	187	219	88.55	51.66	77

2019-086 Kuaizhou-1A Taiyuan Space Centre						2019 Dec 7, 02:55
Jilin-1 High Resolution 02B 2019-086A 44836					in space
Chinese high resolution, multi-spectral imaging satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 07, 04:21	6916	0.0010	531	544	95.39	97.54	267	10:01
2019 Dec 08, 23:28	6917	0.0010	532	546	95.43	97.54	263	10:01

Kuaizhou-1A upper stage 2019-086B 44837					Re-entered - 2020 Mar 4 Life 88 days
Launched Jilin-1 02B. Orbit perigee lowered after releasing the satellite in order to speed up re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 07, 05:54	6850	0.0416	187	756	94.03	97.52	158

2019-087 Kuaizhou 1A Taiyuan Space Centre						2019 Dec 7, 08:52
Head 2 2019-087A 44838					in space
Application satellite from Head Aerospace in the Skywalker constellation, carrying an AIS receiver and providing communications betweeninternet-connected devices.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 07, 11:50	6881	0.0012	495	511	94.68	97.37	268	16:00

Head 3 2019-087B 44839					in space
Application satellite from Head Aerospace in the Skywalker constellation, carrying an AIS receiver and providing communications betweeninternet-connected devices.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 07, 17:47	6881	0.0011	495	511	94.68	97.37	265	16:00

Tianyi 16 2019-087C 44840					in space
Medium resolution optical Earth-imaging satellite. Catalogue number and designation to be confirmed,
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 07, 11:49	6880	0.0010	496	509	94.66	97.38	268	16:00

Tianyi 17 2019-087D 44841					in space
Medium resolution optical Earth-imaging satellite. Catalogue number and designation to be confirmed,
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 07, 17:47	6880	0.0009	496	508	94.66	97.37	260	16:00

Tianqi 4 A 2019-087E 44842					in space
Comsat providing messaging communication links from LEO including between Internet-connected items. Catalogue number and designation to be confirmed,
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 08, 15:53	6880	0.0011	495	509	94.66	97.37	267

Tianqi 4 B 2019-087F 44843					in space
Comsat providing messaging communication links from LEO including between Internet-connected items. Catalogue number and designation to be confirmed,
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 08, 15:53	6880	0.0011	494	510	94.66	97.37	272

Kuaizhou-1A upper stage 2019-087G 44844					in space
Launched group of six satellites. Orbit perigee lowered after releasing the satellite in order to speed up re-entry.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 07, 22:57	7049	0.0657	208	1134	98.17	97.38	341

2019-088 Soyuz-2 1B + Fregat Plesetsk Cosmodrome						2019 Dec 11, 08:54
Cosmos 2544 (Uragan-M) 2019-088A 44850					in space
GLONASS-M navigation satellite to fill a space in the constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 15:17	25516	0.0005	19126	19150	676.05	64.84	264
2019 Dec 19, 12:06	25455	0.0029	19003	19150	673.62	64.83	249

Volga rocket stage 2019-088B 44851					in space
Launched Cosmos 2544. Separated from Soyuz third stage at 09:04 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 15:23	25708	0.0071	19147	19513	683.70	64.81	62

2019-089 PSLV C-48 (QL version) Satish Dhawan Space Centre						2019 Dec 11, 09:55
NANOVA 2019-089A 44852					in space
3U Cubesat acting as demonstrator for the on-orbit element of "Commtrails", a project to create a search and rescue system using direct satellite links for data, voice and text messaging for emergency communications from remote areas. Built by Tyvak for Israeli company Elbit.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 12, 02:49	6947	0.0007	564	574	96.04	36.96	348

RISat 2BR1 (Radar Imaging Satellite) 2019-089B 44853					in space
Indian remote sensing satellite equipped with an imaging radar. Catalogue number and designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 17:18	6948	0.0007	564	574	96.05	36.97	337

Duchifat 3 2019-089C 44854					in space
3U Cubesat for remote sensing, developed by students of the Herzliya Science Centre Space Laboratory, Israel. Catalogue number and designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 17:18	6948	0.0009	564	577	96.07	36.97	326

Lemur-2 (JPGSquared) 2019-089D 44855					in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and a receiver that uses occultation measurements of GPS satellite signals to measure temperature, pressure and humidity profiles in the Earth's atmosphere for weather forecasting. Developed by Spire (formerly Nanosatisfi). One of four Lemur-2 satellites carried on this launch. In order to avoid clutter the others are not listed separately. All are in similar orbits.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 17:18	6949	0.0007	566	576	96.09	36.97	314

Isanagi (QPS-SAR) 2019-089E 44856					in space
Japanese radar-carrying Earth observation satellite from the qPS institute.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 17:18	6951	0.0007	567	578	96.12	36.96	303

Pathfinder Technology Demonstrator 1 2019-089F 44857					in space
6U Cubesat (3x2) - NASA technology demonstrator for a water-based, low thrust, propulsion system. Project led by NASA Ames Research Center in collaboration with NASA Glenn Research Center. First of five planned PDT launches. Catalogue number and designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 19:00	6951	0.0008	568	578	96.13	36.97	297

1HOPSat (First Generation High Optical Performance Satellite) 2019-089G 44858					in space
12U (2x2x3) Cubesat carrying a commercially operated Earth imaging system. Catalogue number and designation to be confirmed.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 19:03	6952	0.0008	569	579	96.15	36.96	280

PSLV upper stage 2019-089L 44862					in space
Launched RISat 2BR1 and nine small satellites. Orbit perigee lowered after releasing final satellite.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 11, 18:47	6923	0.0037	519	571	95.55	36.98	98

2019-090 CZ 3B + YZ-1 Xichang Space Centre						2019 Dec 16, 07:12
Beidou-3 M-19 2019-090A 44864					in space
Phase 2 operational satellite in China's navigation satellite system. One of the final pair needed to complete the Beidou-3, 24 satellite, MEO constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 16, 14:19	28235	0.0119	21521	22193	786.94	55.02	178
2019 Dec 20, 08:42	28077	0.0063	21522	21877	780.36	55.02	184
2019 Dec 24, 15:10	27906	0.0013	21491	21565	773.23	55.01	255

Beidou-3 M-20 2019-090B 44865					in space
Phase 2 operational satellite in China's navigation satellite system. One of the final pair needed to complete the Beidou-3, 24 satellite, MEO constellation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 16, 13:55	28239	0.0118	21528	22193	787.09	55.01	178
2019 Dec 21, 04:01	28197	0.0102	21530	22108	785.35	55.00	179
2020 Jan 20, 23:24	27906	0.0013	21493	21563	773.23	55.04	277

YZ-1 rocket stage 2019-090C 44866					in space
Launched Beidou-3 M-19 and Beidou-3 M-20.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 16, 13:27	28756	0.0065	22190	22565	808.81	54.82	356

CZ 3B upper stage 2019-090D 44867					in space
Launched Beidou-3 M-19 and Beidou-3 M-20.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 16, 10:42	15682	0.5810	192	18416	325.74	55.00	170

2019-091 Falcon 9 Block 5 Cape Canaveral						2019 Dec 17, 00:10
JCSat 18/Kacific 1 2019-091A 44868					in space
Comsat serving east Asia. Two part payload owned jointly by Sky Perfect of Japan and Kacific of Singapore. Expected location 150° east.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Dec 17, 12:28	16677	0.6012	273	20324	357.21	26.91	178
2019 Dec 20, 18:00	21052	0.6825	305	29043	506.64	26.64	179
2019 Dec 31, 14:02	42168	0.0003	35779	35801	1436.26	0.08	28	150° east

Falcon 9 upper stage 2019-091B 44869					in space
Launched JCSat 18/Kacific 1
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 17, 12:27	16673	0.6012	270	20319	357.08	26.91	178

2019-092 Soyuz-ST A + Fregat-M Centre Spatiale Guyanaise						2019 Dec 18, 08:54
CSG-1 (COSMO-SkyMed Second Generation) 2019-092A 44873					in space
Italian Space Agency second generation, follow-on, Earth imaging satellite equipped with synthetic aperture radar. Precise launch time 08:54:20 UTC. Released from Fregat at 09:17:03 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 18, 18:42	7000	0.0001	622	623	97.15	97.82	354	17:50

CHEOPS (Characterising Exoplanet Satellite) 2019-092B 44874					in space
ESA mission to search for exoplanetary transits by performing ultra-high precision photometry on bright stars already known to host planets. Precise launch time 08:54:20 UTC. Released from Fregat at 11:19:01 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 18, 18:53	7081	0.0008	698	709	98.84	98.23	304	17:49

ANGELS (Argos Néo on a Generic Economical and Light Satellite) 2019-092D 44876					in space
12U Cubesat (3x2x2) from French national space agency CNES, fitted with a miniaturized ARGOS Néo instrument, ten times smaller than previous versions. It collects and determines the position of low-power signals and messages from ground-based ARGOS beacons. Precise launch time 08:54:20 UTC. Released from Fregat at 13:07:34 UTC.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 18, 23:19	6895	0.0011	510	525	94.97	97.45	288	17:48

EyeSat 2019-092E 44877					in space
3U Cubesat from France's CNES, equipped with a small telescope designed to study the zodiacal light and to produce images of the Milky Way. Precise launch time 08:54:20 UTC. Released from Fregat at 13:05:04 UTC along with OPS-SAT.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 18, 23:19	6895	0.0013	508	525	94.95	97.44	293	17:48

OPS-SAT 2019-092F 44878					in space
3U Cubesat - ESA mission carrying a 'sandbox' computer to act as in-orbit testbed for new software, new applications and new techniques in satellite control. Precise launch time 08:54:20 UTC. Released from Fregat at 13:05:04 UTC along with EyeSat.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 19, 00:04	6899	0.0010	514	528	95.05	97.47	274	17:48

2019-093 CZ 4B Taiyuan Space Centre						2019 Dec 20, 03:22
ETRSS 1 (Ethiopia Remote Sensing Satellite) 2019-093A 44879					in space
Chinese financed and built satellite operated by Ethiopia, carries high resolution imaging system for remote sensing. Catalogue number, designation and orbit subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 20, 08:05	7003	0.0015	615	636	97.21	97.97	263	10:31

Shuntian 2019-093B 44880					in space
One of pair of communication satellites with a military connection. Testing inter-satellite network links with Yuheng, carried on the same launch. Catalogue number, designation and orbit subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:04	7003	0.0014	615	635	97.21	97.97	264

TianQin 1 2019-093C 44881					in space
Test satellite carrying a micro-thruster for potential use in China's upcoming gravity wave studies satellites. Also carries an Amateur Radio receiver/transmitter.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:05	7003	0.0014	615	635	97.21	97.98	261

Tianyian 01 2019-093D 44882					in space
6U Cubesat equipped with a video Earth imaging system. Catalogue number, designation and orbit subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:05	7003	0.0015	614	636	97.20	97.98	267

CBERS 4A (Ziyuan-1 04B, China-Brazil Earth Resources Satellite) 2019-093E 44883					in space
China-Brazil Earth Resouces Satellite carrying a range of Earth observation sensors. Brazilian built using Chinese satellite bus.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	desc node local time
2019 Dec 27, 19:37	7003	0.0002	623	626	97.20	97.98	85	10:31

Tianyian 02 2019-093F 44884					in space
High resolution Earth imaging satellite. Catalogue number, designation and orbit subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:05	7002	0.0012	615	632	97.18	97.97	248

FloripaSat 2019-093G 44885					in space
1U Cubesat developed by SpaceLab students at the Federal University of Santa Catarina (UFSC), Brazil as a technology demonstrator. Includes an amateur radio package.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:02	7001	0.0013	614	633	97.17	97.98	274

BDS-AGR (BDS Agricultural Company satellite) 2019-093H 44886					in space
Remote sensing satellite for agriculture and crop studies. Catalogue number, designation and orbit subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:05	7000	0.0014	612	632	97.15	97.97	280

Yuheng 2019-093J 44887					in space
One of a pair of communication satellites with a military connection. Testing inter-satellite network links with Shuntian, carried on the same launch. Catalogue number, designation and orbit subject to confirmation.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 08:04	7000	0.0014	612	632	97.14	97.97	280

CZ 4B upper stage 2019-093K 44888					in space
Launched CBERS 4A and other payloads. Orbit perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 12:23	6912	0.0125	447	620	95.31	97.88	20

2019-094 Atlas V N22 Cape Canaveral						2019 Dec 20, 11:36
Boeing Starliner OFT 1 2019-094A 44900					Re-entered - 2019 Dec 22 Life 2 days Returned to Earth
Orbital Flight Test - first test mission for new vehicle to be used for ferrying crew and cargo to/from ISS, no crew carried on this mission. On separation from launch vehicle, Starliner received sufficient thrust to enter very low orbit but software problem prevented major thruster firing and caused it to use up propellant on unnecessary attitude control, leaving insufficient for ISS rendezvous. Retro-fire Dec 22 at 12:01 UTC led to touchdown 12:58 UTC at White Sands Space Harbor, New Mexico, USA.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 20, 11:59	6512	0.0088	76	191	87.16	51.63	323
2019 Dec 20, 13:30	6578	0.0031	180	221	88.50	51.59	239
2019 Dec 20, 14:52	6580	0.0029	182	221	88.52	51.59	237
2019 Dec 20, 17:58	6581	0.0028	184	221	88.54	51.59	240
2019 Dec 21, 08:38	6631	0.0018	241	265	89.57	51.58	198
2019 Dec 21, 20:54	6632	0.0011	246	261	89.57	51.59	291

Atlas V upper stage (Centaur)					Re-entered - 2019 Dec 20 Life <1 day
Launched Boeing Starliner OFT 1. Followed low-perigee orbit similar to the initial one of Starliner itself. Re-entered the atmosphere above southern Pacific Ocean around one hour after lift off. Not catalogued.
Not Catalogued - orbit parameters unavailable

2019-095 Proton-M + DM-03 Baikonur Cosmodrome						2019 Dec 24, 12:03
Elektro L-3 2019-095A 44903					in space
Second generation Russian geosynchronous metsat providing a multispectral image of the complete visible hemisphere every 30 minutes with the interval increased to 15 minutes to cope with emergencies. The satellite also carries a COSPAS-SARSAT search and rescue system receiver. Expected location 165°.8 east.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Dec 24, 23:24	41848	0.0023	35371	35568	1419.93	0.58	231	93° east
2020 Jan 08, 04:47	42065	0.0027	35573	35801	1431.00	0.54	38	145° east
2020 Jan 21, 06:45	42066	0.0027	35572	35802	1431.03	0.51	42	162° east

DM-03 rocket stage 2019-095A 44904					in space
Launched Elektro L-3. Initial orbit shown is an estimate of the one immediately after the first engine firing.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 24, 12:21	6562	0.0010	177	191	88.18	51.56	80
2019 Dec 27, 09:45	41424	0.0084	34697	35394	1398.40	0.46	30

2019-096 Rockot + Briz-KM Plesetsk Cosmodrome						2019 Dec 26, 23:11
Gonets M-14 2019-096A 44905					in space
Store/Dump messaging comsat.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 27, 05:02	7880	0.0005	1498	1506	116.03	82.53	316

Gonets M-15 2019-096B 44906					in space
Store/Dump messaging comsat.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 27, 04:58	7881	0.0005	1499	1507	116.05	82.53	331

Gonets M-16 2019-096C 44907					in space
Store/Dump messaging comsat.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 27, 03:02	7882	0.0005	1500	1508	116.08	82.53	343

BLITS-M (Ball Lens In The Space)					in space
Spherical, 22cm cm diameter glass ball to act as laser retro reflector for use in making high precision geodetic measurements. Reportedly failed to separate from the launch vehicle.
failed to separate from rocket

RS-44 + Briz-KM rocket stage 2019-096E 44909					in space
Launched three Gonets-M satellites and BLITS-M. Also carried attached RS-44 amateur radio transponder that remained intentionally attached to the rocket. Lowered orbit after releasing the Gonets M satellites.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 27, 06:16	7720	0.0209	1180	1504	112.52	82.52	270

2019-097 CZ 5 Wenchang Space Centre						2019 Dec 27, 12:45
Shijian 20 2019-097A 44910					in space
Chinese comsat carried on the 'return to flight' mission of CZ 5 following its launch failure in 2018.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Dec 27, 18:09	40305	0.8373	179	67674	1342.12	19.40	194
2020 Jan 08, 02:48	42164	0.0005	35763	35808	1436.04	0.14	25	115° east

CZ 5 upper stage 2019-097B 44911					in space
Launched Shijian 20.
epoch (UTC)	s-m axis ( km )	ecc	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2019 Dec 27, 20:04	43399	0.8468	269	73772	1499.59	18.32	195