Launch times are in UTC and are either from the launching agency or estimated by 'walking back' along the ground track to the launch site. Most orbit data and decay information comes from SpaceTrack. The Space-Track data occasionally contains inconsistencies (eg - incorrect re-entry dates or early sets of elements allocated to the wrong object) that need to be corrected from other sources.

To fill the gaps where elements are not formally published, usually because they have a classification of "Secret", some orbits are based on amateur observations. Such data is published near-daily by Mike McCants. Occasionally, orbits are estimated by myself from public data.

Space-Track sometimes has insufficient information to allocate names to objects in its catalogue. In these cases, names are derived from public information.

Apogee and perigee are measured against a spherical Earth with a radius of 6378.145 km, assumed to be situated at the focus of the orbital ellipse. The value for the orbital period is the Anomalistic Period, or time to complete one circuit of the ellipse. It is not the same as the time taken to complete one circuit of the Earth. Care should be exercised when comparing Orbital Focus data with other published orbits because they may have been derived using a different model.

Users can go straight to specific launches by pointing to the page URL followed by the three digit launch number, eg - https://www.OrbitalFocus/Diaries/Launches/Launches.php?year=2017#001

You can keep up to date with changes or mission events by following Orbital Focus at Blue Sky.

2017-001 CZ 3B Xichang Space Centre						2017 Jan 5, 15:18
Tongxin Jishu Shiyan 2 (Communication Technology Test 2, TJS 2) 2017-001A 41911						in space
Chinese satellite described as being for communications experiments. May actually be a military Signals Intelligence (SIGINT) satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jan 6, 03:38	24381	0.7301	203	35802	631.44	27.47	180
2017 Jan 16, 22:19	42164	0.0002	35779	35793	1436.06	1.00	119	107°.5 E
2023 Feb 13, 02:29	42164	0.0004	35771	35801	1436.07	0.15	147	66°.5 E
CZ 3B fourth stage 2017-001B 41912						Re-entered - 2020 Jan 21 Life 1111 days
Launched TJS 2.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 5, 20:49	23629	0.7231	164	34338	602.47	27.46	179

2017-002 Kuaizhou 1A Jiuquan Space Centre						2017 Jan 9, 04:11
Xingyun 1 2017-002A 41913						Re-entered - 2024 May 15 Life 2683 days
3U Cubesat testing communication downlinks for future internet comsat constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 9, 19:58	6917	0.0011	531	546	95.41	97.54	269
2023 Feb 13, 09:19	6878	0.0011	492	507	94.61	97.27	138
Jilin-1 Smart Video 03 (Jilin-1 SP03) 2017-002B 41914						in space
Chinese commercial imaging satellite providing high definition Earth surface video. Named after the city where the satellites were developed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Jan 9, 17:05	6916	0.0010	531	545	95.41	97.54	268	10:29
2023 Feb 13, 14:45	6907	0.0012	520	536	95.20	97.26	160	07:44
Kaidun 1 2017-002C 41915						in space
2U Cubesat fitted with an AIS receiver to monitor shipping movements.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 10, 03:52	6914	0.0009	530	542	95.35	97.54	283
2023 Feb 13, 13:59	6895	0.0010	510	523	94.95	97.26	151
Kuaizhou 1A third stage 2017-002D 41916						Re-entered - 2017 Jul 17 Life 189 days
Launched Linye 1 and Jilin-1-03.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 9, 17:57	6770	0.0206	252	531	92.39	97.54	75

2017-003 Falcon 9 v1.2 Vandenberg Air Force Base						2017 Jan 14, 17:54
Iridium 106 (Iridium Next) 2017-003A 41917						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 16, 11:22	6995	0.0009	611	623	97.03	86.67	238
2017 Jan 25, 09:09	7081	0.0003	700	705	98.83	86.53	137
2017 Feb 14, 12:11	7156	0.0002	776	779	100.40	86.40	68
Iridium 103 (Iridium Next) 2017-003B 41918						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 16, 10:17	6995	0.0009	610	623	97.03	86.67	237
2017 Jan 29, 09:06	7081	0.0002	702	705	98.84	86.53	121
2017 Feb 22, 15:48	7155	0.0010	770	784	100.39	86.41	115
2017 Feb 24, 07:59	7156	0.0002	776	780	100.41	86.39	60
Iridium 109 (Iridium Next) 2017-003C 41919						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 16, 10:17	6995	0.0009	610	623	97.03	86.67	234
2017 Jan 28, 01:35	7081	0.0002	701	704	98.83	86.52	116
2017 Feb 16, 12:36	7155	0.0003	774	779	100.38	86.39	53
2017 Feb 20, 03:40	7156	0.0003	776	780	100.40	86.39	69
Iridium 102 (Iridium Next) 2017-003D 41920						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 16, 11:22	6994	0.0009	610	623	97.02	86.67	233
2017 Jan 30, 14:39	7082	0.0002	703	705	98.86	86.52	49
2017 Mar 19, 19:39	7156	0.0003	776	779	100.40	86.39	77
Iridium 105 (Iridium Next) 2017-003E 41921						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 16, 11:22	6994	0.0009	609	623	97.02	86.67	233
2018 Feb 22, 12:28	7083	0.0003	702	707	98.87	86.15	144
2018 Feb 26, 12:57	7156	0.0003	775	780	100.40	86.39	119
Iridium 104 (Iridium Next) 2017-003F 41922						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 16, 11:22	6994	0.0010	609	622	97.01	86.67	231
2017 Mar 10, 21:38	7156	0.0002	776	779	100.40	86.39	99
Iridium 114 (Iridium Next) 2017-003G 41923						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 16, 11:22	6993	0.0010	608	622	97.01	86.67	229
2017 Feb 6, 15:24	7083	0.0002	703	706	98.87	86.53	101
2017 Mar 5, 19:33	7156	0.0002	776	779	100.40	86.39	96
Iridium 108 (Iridium Next) 2017-003H 41924						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 16, 11:22	6993	0.0010	608	622	97.00	86.67	224
2017 Aug 30, 09:11	6994	0.0012	608	624	97.03	85.89	149
2018 Feb 26, 13:06	7155	0.0003	775	779	100.40	86.39	101
Iridium 112 (Iridium Next) 2017-003J 41925						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 16, 13:35	6993	0.0009	609	621	97.00	86.66	228
2017 Feb 16, 14:10	7081	0.0002	701	705	98.84	86.53	125
2017 Mar 12, 03:37	7156	0.0005	774	782	100.41	86.38	52
Iridium 111 (Iridium Next) 2017-003K 41926						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 16, 13:36	6993	0.0010	608	622	97.00	86.67	225
2017 Feb 14, 01:10	7081	0.0002	701	705	98.84	86.53	120
2017 Mar 23, 20:37	7156	0.0002	776	779	100.40	86.39	94
Falcon 9 upper stage uncatalogued						Re-entered - 2017 Jan 14 Life <1 day
Launched cluster of ten Iridium Next satellites. Caused to re-enter soon after launch. Not catalogued.
Not Catalogued - orbit parameters unavailable

2017-F01 - failed to reach orbit SS-520 Uchinoura Space Center, Japan						2017 Jan 14, 23:33
Tricom 1
3U Cubesat from the University of Tokyo carring an Earth imaging camera and a store and forward messaging payload. Mission was a demonstration of the SS-520 sounding rocket, with an added third stage, as a satellite launcher. Lost when controllers lost communication with the SS-520 and it failed to reach orbit.

2017-I01 JEM Small Satellite Orbital Deployer International Space Station						2017 Jan 16, 09:10
Freedom 1998-067KS 41930						Re-entered - 2017 Feb 5 Life 20 days
1U CubeSat developed by Nakashimada Engineering Works and Tohoku University to demonstrate a deployable deorbit saill for space debris mitigation. Its relatively short 20 day lifetime indicates that the sail worked as planned.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 18, 05:04	6778	0.0008	395	405	92.56	51.64	70
ITF-2 1998-067KU 41932						Re-entered - 2019 Jan 3 Life 717 days
1U Cubesat built by students of the University of Tsukuba to test a small antenna and to test the use of a microelectronic package to control a satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 18, 03:32	6781	0.0007	398	408	92.62	51.64	69
Waseda-Sat 3 1998-067KV 41933						Re-entered - 2018 Oct 6 Life 628 days
1U Cubesat from Waseda University, fitted with an ultra light drag parachute to accelerate orbital decay.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 18, 03:32	6781	0.0008	398	408	92.62	51.64	63

2017-I02 JEM Small Satellite Orbital Deployer International Space Station						2017 Jan 16, 09:20
EGG (e-Entry satellite with Gossamer aeroshell and GPS/Iridium) 1998-067KW 41934						Re-entered - 2017 May 15 Life 119 days
2U Cubesat from the University of Tokyo, equipped with a deployable lightweight aeroshell to accelerate re-entry, and using GPS for position fixing, and a comms package using Iridium satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 18, 05:05	6781	0.0009	397	409	92.62	51.64	78

2017-I03 JEM Small Satellite Orbital Deployer International Space Station						2017 Jan 16, 10:40
AOBA-Velox 3 1998-067KX 41935						Re-entered - 2018 Nov 1 Life 654 days
2U Cubesat developed by Nanyang Technological University of Singapore and the Kyushu Institute of Technology of Japan to demonstrate a Pulsed Plasma Thruster（PPT） for attitude control and orbit maintenance, and test a Bluetoth communications system between satellite components.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 18, 05:05	6781	0.0007	399	408	92.62	51.64	76

2017-I04 JEM Small Satellite Orbital Deployer International Space Station						2017 Jan 16, 10:50
Tancredo 1 1998-067KT 41931						Re-entered - 2017 Oct 18 Life 275 days
Tubesat developed by students from the Tancredo Almeida Neves school, Ubatuba, Brazil. Equipped with avoice recorder for radio-amateur use, and a simple Langmuir probe to study the formation of plasma bubbles in the ionosphere. Released from TuPOD 2017 Jan 18 at about 01:00 UTC, around 38 hours after it left ISS.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 17, 22:55	6781	0.0009	396	409	92.61	51.64	73
TuPOD (Tubesat Picosat Orbital Deployer) 1998-067KY 41936						Re-entered - 2017 Sep 8 Life 235 days
Tubesat deployer designed by Italy's GAUSS (Astrodynamics Group for the Use of Space Systems) with the form factor of a 3U Cubesat. Released two Tubesats after being launched from the ISS. Carried amatur radio morse code transmitter to indicate its presence.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 21, 02:29	6781	0.0009	396	408	92.61	51.64	83
OSNSat 1998-067KZ 41939						Re-entered - 2018 Jan 11 Life 360 days
Tubesat developed by the Open Space Network company, California. Purpose unknown. Released from TuPOD 2017 Jan 18 at about 01:00 UTC, around 38 hours after it left ISS.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 21, 19:27	6780	0.0010	395	408	92.60	51.65	80

2017-004 Atlas V 401 Cape Canaveral Air Force Station						2017 Jan 21, 00:42
USA 273 (SBIRS GEO 3) 2017-004A 41937						in space
Missile launch detection satellite for the Space-Based Infra Red System with a combination of scanning and staring sensors. The scanning sensor is designed to provide a wide area view in search of missile launches, satellite re-entries and natural terrestrial events, while the staring sensor is designed to observe areas of particular interest with enhanced sensitivity. Separated from the launch vehicle at 01:25 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jan 22, 19:30	24370	0.7302	196	35787	631.01	23.25	179
2017 Jan 28, 15:54	26606	0.5812	4764	35692	719.83	15.80	182
2017 Jan 30, 18:23	29084	0.4445	9777	35634	822.68	12.07	183
2017 Feb 2, 16:50	33220	0.2628	18111	35572	1004.29	8.86	183
2017 Feb 4, 07:13	34625	0.2110	20942	35552	1068.67	8.17	183
2017 Feb 6, 22:53	35186	0.1915	22071	35545	1094.75	7.93	183
2017 Feb 11, 22:56	36274	0.1555	24254	35537	1145.90	7.53	183
2017 Feb 14, 23:37	38236	0.0960	28188	35528	1240.13	6.93	183
2017 Feb 20, 17:29	40308	0.0395	32338	35522	1342.31	6.41	184
2017 Mar 11, 14:50	42168	0.0025	35683	35897	1436.25	5.99	358	158°.9 W
2023 Feb 12, 19:07	42165	0.0002	35777	35796	1436.09	1.91	359	159°.4 W
Atlas V upper stage (Centaur) 2017-004B 41938						Re-entered - 2019 Nov 19 Life 1032 days
Launched USA 273
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 22, 17:03	24437	0.7320	171	35947	633.62	22.98	178

2017-005 H-IIB (F-32) Tanegashima Space Centre						2017 Jan 24, 07:44
Kirameki 2 (DSN 2) 2017-005A 41940						in space
Military comsat operated by DSN Corporation, a subsidiary of SKY Perfect JSAT Group, used by the Japanese military. Expected location - Indian Ocean region. Orbit based on amateur observations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Apr 29, 07:51	42165	0.0005	35764	35810	1436.12	0.02	225	93°.1 E
H-IIA upper stage 2017-005B 41941						in space
Launched DSN 2. Orbit parameters based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2018 Aug 1, 13:34	24215	0.7219	357	35318	625.03	21.31	205

2017-006 Soyuz ST-B + Fregat-MT (VS-16) Centre Spatiale Guyanaise						2017 Jan 28, 01:03
Hispasat 36W-1 2017-006A 41942						in space
Spanish comsat providing telephone and TV services to Europe and north Africa. Precise launch time 01:03:34 UTC. Separated from launch vehicle at 01:35:44 UTC. Expected location 36° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jan 29, 04:17	24388	0.7276	266	35754	631.71	5.43	179
2017 Feb 10, 13:32	42164	0.0002	35779	35792	1436.04	0.09	74	26°.0 W
2017 May 11, 10:26	42165	0.0004	35771	35802	1436.09	0.05	323	26°.0 W
2017 May 17, 10:26	42250	0.0002	35863	35881	1440.45	0.07	330
2017 May 22, 10:22	42164	0.0000	35784	35788	1436.06	0.08	355	35°.8 W
2023 Feb 12, 16:16	42165	0.0001	35782	35791	1436.09	0.04	30	36°.0 W
Fregat rocket stage 2017-006B 41943						Re-entered - 2024 Jun 25 Life 2705 days
Launched Hispasat 36W-1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jan 29, 03:45	24286	0.7298	183	35633	627.77	5.46	179

2017-007 Ariane 5ECA (VA-235) Centre Spatiale Guyanaise						2017 Feb 14, 21:39
Telkom 3S 2017-007A 41944						in space
Comsat serving Indonesia, Malaysia and other neighbouring parts of Asia. Separated from the launch vehicle at 22:06 UTC. Replacement for Telkom3 (2012-044A/38744) that was lost when its Proton rocket delivered to an unusable orbit. Expected location - 118° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Feb 14, 16:56	24403	0.7276	269	35780	632.28	4.02	178
2017 Feb 16, 14:05	29465	0.4297	10426	35747	838.91	1.66	178
2017 Feb 18, 23:43	38251	0.1014	27994	35751	1240.84	0.36	175
2017 Feb 19, 14:12	42031	0.0026	35543	35763	1429.26	0.03	140	130°.5 E
2017 Feb 26, 22:08	42163	0.0001	35780	35789	1435.99	0.03	121	135°.6 E
2017 Mar 9, 21:49	42260	0.0012	35832	35931	1440.95	0.03	145
2017 Mar 26, 23:28	42207	0.0005	35809	35850	1438.28	0.05	278	117°.9 E
2017 Mar 30, 20:48	42165	0.0001	35784	35790	1436.12	0.05	173	118°.1 E
2023 Feb 12, 14:58	42165	0.0002	35778	35795	1436.09	0.02	209	118°.0 E
Intelsat 32e (Sky Brasil 1) 2017-007B 41945						in space
Comsat providing TV, cinema and broadband services to Brazil. Sky Brasil is the brand name of the transponders (owned by Yahsat) providing the broadband service. Separated from the launch vehicle at 22:18 UTC. Expected location 43° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Feb 14, 16:59	24398	0.7277	266	35774	632.12	4.02	178
2017 Feb 18, 17:37	37162	0.1335	25821	35746	1188.23	0.67	180
2017 Feb 22, 10:06	42064	0.0016	35620	35752	1430.95	0.09	188	34°.8 W
2017 Feb 27, 14:13	42164	0.0001	35782	35790	1436.06	0.08	85	33°.0 W
2017 Mar 20, 16:48	42244	0.0002	35856	35876	1440.16	0.05	352
2017 Mar 27, 10:16	42245	0.0002	35857	35876	1440.19	0.05	358
2017 Mar 29, 14:11	42164	0.0004	35771	35801	1436.07	0.03	4	43°.2 W
2023 Feb 13, 09:26	42165	0.0000	35787	35787	1436.12	0.02	351	43°.2 W
Ariane 5 upper stage 2017-007C 41946						in space
Launched Intelsat 32e and Telkom 3S.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 14, 16:55	24419	0.7277	271	35810	632.91	4.04	178

2017-008 PSLV-XL (PSLV C-37) Satish Dhawan Space Centre						2017 Feb 15, 03:58
Cartosat 2D 2017-008A 41948						in space
Indian imaging satellite for cartography/mapping.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Feb 15, 23:51	6881	0.0009	497	509	94.68	97.51	249	09:29
2017 Feb 16, 17:14	6891	0.0009	507	520	94.89	97.51	251	09:29
2017 Mar 17, 19:05	6888	0.0009	504	515	94.81	97.51	156	09:30
2017 Mar 19, 12:12	6886	0.0008	503	513	94.79	97.51	159	09:30
2023 Feb 13, 05:26	6886	0.0006	504	512	94.78	97.43	211	09:30
INS 1A (Indian NanoSatellite 1A) 2017-008B 41949						Re-entered - 2023 Oct 3 Life 2421 days
Science satellite from the Indian Space Research Organisation. Payloads include Surface Bidirectional Reflectance Distribution Function Radiometer to measure the eflectance of sunlight from Earth surface features., and the Single Event Upset Monitor to monitor fluctuationsbin high energy radiation in the space environment.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 28, 19:43	6881	0.0010	496	509	94.67	97.51	201
INS 1B (Indian NanoSatellite 1B) 2017-008G 41954						Re-entered - 2023 Oct 13 Life 2431 days
Science satellite from the Indian Space Research Organisation. Payload includes the Earth Exosphere Lyman Alpha Analyser to measure neutral atomic hydrogen and to estimate the level of interplanetary hydrogen Lyman-alpha background radiation, and the Origami Camera - for remote sensing in colour.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 28, 21:16	6880	0.0009	496	508	94.66	97.51	201
2023 Feb 13, 11:10	6819	0.0007	437	446	93.41	97.22	91
Flock 3P-1 2017-008V 41967						Re-entered - 2022 Nov 8 Life 2092 days
3U Cubesat, part of Planet's Flock 3P cluster of imaging satellites. Flock 3P-1 is one of a swarm of 88 similar satellites carried on this launch, 2017-008. To avoid clutter, the others are not listed separately. All satellites are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 28, 18:04	6880	0.0008	496	507	94.65	97.51	204
Lemur-2 (Satchmo) 2017-008AV 41991						Re-entered - 2023 Jul 11 Life 2337 days
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). Lemur-2 satellites are named after development and support team members. One of a cluster of eight Lemur-2 satellites carried on this launch, 2017-008. To avoid clutter, the others are not listed separately. All satellites are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 28, 19:35	6879	0.0007	496	505	94.63	97.51	206
2023 Feb 13, 10:21	6809	0.0005	428	435	93.20	97.23	92
BGUSat 2017-008BD 41999						Re-entered - 2023 Feb 24 Life 2200 days
3U Cubesat from Ben Gurion University, Israel. Student project to explore atmospheric and weather phenomena at Infra-red frequencies.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 1, 17:39	6878	0.0008	495	505	94.62	97.51	221
2023 Feb 13, 04:53	6680	0.0004	299	305	90.56	97.24	316
Dido 2 2017-008BE 42000						Re-entered - 2024 Jul 12 Life 2704 days
3U Cubesat carrying microgravity experiments from a co-operation between Spacepharma of Israel and a range of Chinese organisations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 28, 11:40	6878	0.0007	495	505	94.62	97.51	226
PEASSS (Piezoelectric Assisted Smart Satellite Structure) 2017-008BV 42015						Re-entered - 2023 Dec 1 Life 2480 days
3U Cubesat to test test and qualify 'smart structures' which combine composite panels, piezoelectric materials, and next generation sensors, for improved satellite pointing accuracy and power generation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 28, 17:52	6877	0.0005	495	502	94.59	97.51	231
Al-Farabi 1 2017-008BW 42016						Re-entered - 2023 Jul 25 Life 2351 days
2U Cubesat from Al-Farabi Kazakh National University.Technology demonstration satellite built to support the university's education programme.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 28, 02:05	6877	0.0005	495	502	94.59	97.51	235
2023 Feb 13, 10:57	6801	0.0004	420	425	93.03	97.24	102
Nayif 1 (Emirates-OSCAR 88) 2017-008BX 42017						Re-entered - 2023 Jul 20 Life 2346 days
1U Cubesat from the United Arab Estimates. Project from the Emirates Institution for Advanced Science and Technology the American University of Sharjah aimed at developing the capabilities of Emirati engineering students. Payload includes the FUNCube 5 amateur radio package.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 28, 02:05	6877	0.0005	495	502	94.58	97.51	234
2023 Feb 13, 02:43	6800	0.0004	419	424	93.00	97.24	101
PSLV upper stage 2017-008DJ 42052						Re-entered - 2024 Oct 6 Life 2790 days
Launched Cartosat 2D, two other small satellites and and 101 Cubesats.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 28, 04:22	6864	0.0015	475	496	94.32	97.51	47

2017-009 Falcon 9 v1.2 Kennedy Space Center						2017 Feb 19, 14:39
SpaceX Dragon CRS-10 2017-009A 42053						Re-entered - 2017 Mar 19 Life 28 days Returned to Earth
Carrying a cargo to the ISS under NASA's Commercial Resupply Services (CRS) contract. An initial approach to the ISS 2017 Feb 22 was aborted because of an error in Dragon's navigation system. Captured by the ISS Remote Manipulator System Feb 23 at 10:44 UTC and attached to th lower port of the Harmony module at 13:12 UTC. Undocked using the RMS 2017 Mar 18 at 21:20 UTC. Released Mar 19 at 09:11 UTC. Retro-fire at 14:01 UTC led to splashdown at 14:46 UTC in the Pacific Ocean, about 300 km SW of Baja, California.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 19, 17:58	6660	0.0117	204	360	90.16	51.63	46
2017 Feb 21, 19:18	6771	0.0005	389	397	92.42	51.65	218
2017 Feb 22, 21:31	6788	0.0018	397	421	92.75	51.56	343
2017 Feb 23, 06:42	6782	0.0007	399	408	92.64	51.64	221
Falcon 9 upper stage uncatalogued						Re-entered - 2017 Feb 19 Life <1 day
Launched SpaceX Dragon CRS-10. Re-entered soon after launch. Not catalogued.
Not Catalogued - orbit parameters unavailable

2017-010 Soyuz-U 11A511U Baikonur Cosmodrome						2017 Feb 22, 05:58
Progress MS-05 (Progress 7K-MS №435) 2017-010A 42056						Re-entered - 2017 Jul 20 Life 148 days
Supplies to ISS. Docked with the port on the ISS Pirs module 2017 Feb 24 at 08:34 UTC. Undocked 2017 July 20 at 17:46 UTC. Retrofire at 20:58 UTC resulted in a destructive re-entry at 21:32 UTC with any surviving fragments impacting the southern Pacific Ocean at 21:41 UTC. Final launch using Soyuz-U variant of the launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 22, 07:59	6584	0.0020	193	218	88.61	51.59	93
2017 Feb 23, 16:23	6683	0.0014	296	314	90.61	51.64	162
2017 Feb 25, 13:16	6782	0.0006	399	408	92.64	51.64	235
Soyuz upper stage 2017-010B 42057						Re-entered - 2017 Feb 24 Life 2 days
Launched Progress MS-05.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Feb 22, 06:27	6577	0.0018	187	211	88.47	51.62	80

2017-011 Atlas V 401 Vandenberg Air Force Base						2017 Mar 1, 17:49
USA 274 p/l 1 (NOSS 3-8 p/l 1, Intruder) 2017-011A 42058						in space
Navy Ocean Surveillance Satellite (NOSS) - main payload. Orbit is based on amateur observations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 27, 01:43	7484	0.0124	1014	1199	107.40	63.44	179
USA 274 p/l 2 (NOSS 3-8 p/l 2, Intruder) 2017-011B 42065						in space
Navy Ocean Surveillance Satellite (NOSS), second of the satellite pair, released from its parent soon after launch. Orbit is based on amateur observations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 27, 01:43	7484	0.0127	1011	1201	107.40	63.44	179
Atlas V upper stage (Centaur) uncatalogued						Re-entered - 2017 Mar 1 Life <1 day
Caused to re-enter soon after launch. Not catalogued.
Not Catalogued - orbit parameters unavailable

2017-012 Kaituozhe-2 Jiuquan Space Centre						2017 Mar 2, 23:53
Tiankun 1 2017-012A 42061						Re-entered - 2023 Jul 7 Life 2318 days
Technology demonstration satellite for new small satellite bus.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 3, 05:59	6687	0.0137	217	401	90.71	96.68	331
2017 Mar 3, 15:26	6774	0.0016	384	406	92.47	96.93	277
KT-2 upper stage 2017-012B 42062						Re-entered - 2017 Apr 8 Life 37 days
Launched Tiankun 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 3, 07:09	6773	0.0016	384	406	92.46	96.93	279

2017-I06 Nanoracks Cubesat Deployer International Space Station						2017 Mar 6, 10:25
Lemur-2 (Trutna) 1998-067LC 42067						Re-entered - 2018 Apr 15 Life 405 days
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. May not have become stabilised so made an early re-entry. Developed by Spire (formerly Nanosatisfi). Lemur-2 satellites are named after development and support team members.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 8, 18:49	6781	0.0011	396	410	92.62	51.64	321
Lemur-2 (TrutnaHD) 1998-067LE 42069						Re-entered - 2018 Nov 13 Life 617 days
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). Lemur-2 satellites are named after development and support team members.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 8, 18:49	6781	0.0009	397	409	92.62	51.64	284

2017-I07 Nanoracks Cubesat Deployer International Space Station						2017 Mar 6, 15:05
Lemur-2 (Redfern-Goes) 1998-067LA 42059						Re-entered - 2018 Dec 5 Life 639 days
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). Lemur-2 satellites are named after development and support team members.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 8, 15:43	6781	0.0009	397	409	92.61	51.64	284
Lemur-2 (Austintacious) 1998-067LD 42068						Re-entered - 2018 Oct 4 Life 577 days
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). Lemur-2 satellites are named after development and support team members.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 8, 11:17	6781	0.0008	397	408	92.62	51.64	276

2017-I08 Nanoracks Cubesat Deployer International Space Station						2017 Mar 6, 18:20
TechedSat 5 1998-067LB 42066						Re-entered - 2017 Jul 29 Life 145 days
3.5U Cubesat from NASA fitted with Exo-Brake, resembling a configurable, cross-shaped parachute capable of varying its drag to control re-entry.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 8, 18:48	6780	0.0008	396	407	92.60	51.64	290

2017-013 Vega (VV-09) Centre Spatiale Guyanaise						2017 Mar 7, 01:49
Sentinel 2B 2017-013A 42063						in space
Second of of a pair of optical imaging satellites The satellite is part of ESA's Copernicus constellation, the EU contribution to GEOSS (Global Earth Observation System of Systems). Precise launch time: 01:49:24 UTC, separated from the launch vehicle at 02:47:21 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Mar 7, 06:49	7156	0.0001	777	779	100.41	98.56	351	10:29
2017 Mar 9, 19:06	7158	0.0002	778	781	100.44	98.56	25	10:29
2017 Mar 16, 17:26	7160	0.0002	781	783	100.50	98.58	190	10:29
2017 Mar 21, 14:52	7164	0.0005	782	790	100.57	98.58	115	10:29
2017 Mar 23, 18:14	7167	0.0002	787	790	100.63	98.57	76	10:30
2017 Mar 28, 20:45	7167	0.0002	788	790	100.64	98.57	111	10:30
2023 Feb 13, 11:41	7167	0.0001	788	790	100.64	98.56	102	10:30
Vega upper stage (AVUM) 2017-013B 42064						Re-entered - 2017 Mar 7 Life <1 day
Launched Sentinel 2B. De-orbited.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 7, 03:37	7160	0.0016	771	794	100.49	98.54	322

2017-014 Falcon 9 v1.2 Kennedy Space Center						2017 Mar 16, 06:00
Echostar 23 2017-014A 42070						in space
Commercial communications satellite covering Brazil. Expected location 45° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Mar 17, 23:52	24413	0.7316	174	35896	632.68	22.43	180
2017 Mar 18, 23:47	26283	0.6080	3924	35885	706.74	13.69	181
2017 Mar 19, 14:14	29465	0.4343	10289	35885	838.92	7.28	181
2017 Mar 20, 23:00	35223	0.1996	21815	35875	1096.47	2.45	181
2017 Mar 23, 14:39	42037	0.0032	35526	35792	1429.57	0.22	353	43°.5 W
2017 Apr 5, 14:03	42165	0.0002	35778	35796	1436.10	0.07	75	44°.9 W
2023 Feb 12, 12:28	42165	0.0002	35779	35795	1436.10	0.02	222	109°.9 W
Falcon 9 upper stage 2017-014B 42071						Re-entered - 2022 Feb 6 Life 1788 days
Launched Echostar 23.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 16, 22:18	24387	0.7313	176	35842	631.69	22.43	179

2017-015 H-IIA 202 (F-33) Tanegashima Space Centre						2017 Mar 17, 01:20
IGS 11 (IGS Radar 5) 2017-015A 42072						in space
Information Gathering Satellite - Japanese government/military radar imaging reconnaissance satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Mar 30, 21:13	6870	0.0010	485	499	94.46	97.23	357	10:14
2017 Apr 9, 20:41	6866	0.0005	484	491	94.36	97.38	51	10:15
2018 Apr 8, 20:41	6866	0.0003	486	490	94.37	97.37	102	10:15
2019 Apr 10, 21:05	6866	0.0002	486	489	94.37	97.37	2	10:15
2020 Apr 10, 20:17	6866	0.0004	485	490	94.37	97.36	81	10:15
2021 Apr 8, 23:41	6866	0.0003	486	490	94.37	97.37	348	10:14
H-IIA upper stage 2017-015B 42073						Re-entered - 2023 Dec 11 Life 2460 days
Launched IGS 10.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Apr 9, 20:39	6870	0.0010	485	499	94.45	97.20	311

2017-016 Delta 4 Medium+ 5,4 Cape Canaveral Air Force Station						2017 Mar 19, 00:18
USA 275 (Wideband Global SATCOM 9) 2017-016A 42075						in space
Block II Military communications satellite, providing communications links for troops in the field. A major improvent in the Block II satellites is transmission of airborne intelligence, surveillance and reconnaissance imagery at approximately three times the data rate available through the Block I satellites. Operated jointly by the US DoD and the Australian Department of Defense. Separated from launch vehicle at 00:59 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Mar 20, 17:41	28761	0.7619	470	44297	809.05	26.99	179
2017 Mar 31, 19:02	42168	0.2387	25722	45857	1436.24	0.23	294	121°.6 W
2017 Jun 13, 14:33	42214	0.0054	35609	36063	1438.61	0.09	327	120°.8 W
2017 Jun 22, 20:33	42166	0.0000	35787	35789	1436.15	0.07	110	121°.9 W
2023 Feb 12, 20:42	42165	0.0001	35785	35789	1436.13	0.01	266	12°.0 W
Delta 4 upper stage 2017-016B 42076						Re-entered - 2017 Mar 19 Life <1 day
Launched USA 275.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Mar 19, 06:12	26249	0.7642	-189	39931	705.40	26.99	173

2017-017 Falcon 9 v1.2 Kennedy Space Center						2017 Mar 30, 22:27
SES 10 2017-017A 42432						in space
Communications satellite providing coverage of Mexico, other parts of Spanish speaking South America and Brazil, with the ability to support off-shore oil and gas exploration. Launched at the opening of a 150 minute window. Separated from the launch vehicle at 22:57 UTC. Expected location 67° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Apr 1, 20:34	27121	0.5523	5764	35722	740.84	13.16	179
2017 Apr 4, 19:25	39832	0.0570	31185	35723	1318.60	0.79	184
2017 Apr 5, 18:51	42088	0.0005	35690	35729	1432.17	0.10	238	72°.8 W
2017 Apr 12, 15:10	42164	0.0003	35775	35797	1436.08	0.09	152	68°.5 W
2023 Feb 13, 03:37	42165	0.0003	35776	35799	1436.13	0.02	247	66°.9 W
Falcon 9 upper stage 2017-017B 42433						in space
Launched SES 10.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Apr 1, 18:58	23200	0.7149	236	33408	586.12	26.18	179

2017-018 CZ 3B Xichang Space Centre						2017 Apr 12, 11:04
Shijian 13 (Practice 13) 2017-018A 42662						in space
High capacity Chinese comsat covering the mainland and coastal waters. Known as Shijian 13 during its test phase. Expected location 110°.5 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Apr 12, 17:13	27371	0.7581	243	41744	751.11	20.96	179
2017 Apr 25, 02:24	42165	0.0004	35768	35806	1436.11	0.07	144	110°.5 E
2023 Feb 12, 08:52	42165	0.0006	35760	35814	1436.12	0.08	168	110°.5 E
CZ 3B fourth stage 2017-018B 42663						in space
Launched Shijian 13
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Apr 12, 15:20	26752	0.7532	225	40522	725.74	20.96	178

2017-019 Atlas V 401 Cape Canaveral Air Force Station						2017 Apr 18, 15:11
Cygnus OA-7 (SS John Glenn) 2017-019A 42681						Re-entered - 2017 Jun 11 Life 54 days
Resupply mission to ISS. Captured by ISS Remote Manipulator Apr 22 at 10:05 UTC and docked with the downward-facing port on Unity at 12:39 UTC. Undocked using the ISS Remote Manipulator Jun 4 at 11:05 UTC. Released from the manipulator at 13:10 UTC. Ejected four Cubesats Jun 8. Retrofire Jun 11 led to destructive re-entry above the southern Pacific Ocean at around 17:08 UTC any remaining fragments impacted the ocean surface about 10 mins later.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Apr 18, 20:05	6614	0.0002	234	237	89.22	51.65	287
2017 Apr 19, 11:16	6783	0.0010	398	412	92.67	51.65	170
2017 Apr 20, 15:09	6773	0.0011	387	402	92.45	51.64	86
2017 Apr 21, 17:15	6778	0.0006	396	404	92.56	51.64	83
2017 Apr 22, 14:35	6783	0.0007	400	409	92.66	51.64	85
2017 Jun 2, 09:35	6783	0.0005	402	408	92.67	51.64	221
2017 Jun 4, 15:00	6797	0.0019	406	431	92.94	51.62	326
2017 Jun 5, 08:33	6788	0.0004	407	413	92.77	51.64	235
2017 Jun 8, 22:59	6859	0.0007	476	485	94.22	51.64	295
2017 Jun 10, 17:26	6776	0.0009	392	404	92.52	51.64	301
2017 Jun 11, 04:27	6773	0.0012	387	403	92.46	51.64	289
Lemur-2 (Angela) 2017-019B 42752						Re-entered - 2023 Apr 6 Life 2179 days
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). Lemur-2 satellites are named after development and support team members. Released from SS John Glenn 2017 Jun 8 at 17:53 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 12, 20:51	6862	0.0011	476	491	94.28	51.64	331
Lemur-2 (JennyBarna) 2017-019C 42753						Re-entered - 2022 Dec 28 Life 2080 days
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). Lemur-2 satellites are named after development and support team members. Released from SS John Glenn 2017 Jun 8 at 17:53 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 12, 22:25	6862	0.0011	476	491	94.28	51.64	331
Lemur-2 (RobMoore) 2017-019D 42754						Re-entered - 2023 Apr 29 Life 2202 days
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). Lemur-2 satellites are named after development and support team members. Released from SS John Glenn 2017 Jun 8 at 21:03 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 12, 22:26	6862	0.0011	477	491	94.29	51.64	334
Lemur-2 (Spirovision) 2017-019E 42755						Re-entered - 2022 Dec 28 Life 2080 days
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). Lemur-2 satellites are named after development and support team members. Released from SS John Glenn 2017 Jun 8 at 21:03 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 12, 22:26	6862	0.0011	477	491	94.29	51.64	333
Atlas V upper stage uncatalogued						Re-entered - 2017 Apr 18 Life <1 day
Launched SS John Glenn/Cygnus OA-7. Caused to re-enter before it could be catalogued.
Not Catalogued - orbit parameters unavailable

2017-020 Soyuz-FG 11A511U-FG Baikonur Cosmodrome						2017 Apr 20, 07:13
Soyuz MS-04 (Soyuz 11F732A48 № 735) 2017-020A 42682						Re-entered - 2017 Sep 3 Life 136 days Returned to Earth
Carrying crew of two to ISS - Fyodr Yurchikhin (Roscosmos) and Jack Fischer (NASA). Precise launch time 07:13:43 UTC. Docked with the Poisk module of the ISS Apr 20 at 13:23 UTC. Precise launch time 07:13:43 UTC. Undocked, carrying Yurchikin, Fischer and Peggy Whitson 2017 Sep 2 at 21:58 UTC. Retro-fire Sep 3 at 00:29 UTC was followd by landing in Kazakhstan, 148 kilometers south east of Dzhezkazgan, at 01:21 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Apr 20, 11:54	6783	0.0007	400	410	92.66	51.64	77
Soyuz upper stage 2017-020B 42683						Re-entered - 2017 Apr 23 Life 3 days
Launched Soyuz MS-04.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Apr 20, 21:48	6585	0.0026	190	224	88.63	51.62	78

2017-021 CZ 7 (Y-2) Wenchang Space Centre						2017 Apr 20, 11:41
Tianzhou 1 2017-021A 42684						Re-entered - 2017 Sep 22 Life 155 days
Spacecraft to test propellant transfer to China's future large space station. Docked with Tiangong 2 (2016-057A/41765) 2017 Apr 22 at 04:16 UTC with latches engaged at 04:23 UTC. Completed a propellant transfer Apr 27 at 11:07 UTC and completed a second one Jun 15 at 10:28 UTC. Each operation took five days. Undocked 2017 Jun 19 and conducted a fly-around of Tiangong 2. Docked a second time with Tiangong 2 on Jun 19 at about 06:48 UTC with latches angaged at 06:55 UTC. Undocked Jun 21 at 09:47 UTC. Docked with Tiangong 2 for a third time 2017 Sep 12 at about 15:50 UTC after an approach to simulate a short duration launch-docking mission, similar to Soyuz. Latches were engaged at 15:58 UTC. Completed a three-day propellant transfer test Sep 16 at 12:17 UTC. Undocked Sep 17 at 08:15 UTC. Retro-fire Sep 22 at around 12:00 UTC led to destructive re-entry about 45 mins later with any surviving fragments hitting the southern Pacific Ocean.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Apr 20, 20:42	6718	0.0044	311	369	91.33	42.79	181
2017 Apr 21, 17:54	6751	0.0008	367	378	92.00	42.78	276
2017 Apr 22, 16:53	6763	0.0007	380	390	92.25	42.79	289
2017 Jun 14, 14:33	6762	0.0011	377	391	92.23	42.78	314
2017 Jun 19, 13:02	6764	0.0010	379	393	92.28	42.78	2
2017 Jun 21, 13:57	6773	0.0003	393	397	92.45	42.78	274
2017 Sep 11, 06:28	6771	0.0000	393	393	92.41	42.78	104
2017 Sep 12, 06:50	6695	0.0186	193	441	90.86	42.25	230
2017 Sep 13, 07:26	6769	0.0002	390	393	92.38	42.78	167
Silu 1 (Silk Road 1) 2017-021F 42903						Re-entered - 2019 Apr 11 Life 721 days
3U Cubesat carrying development versions of sensors to be used in a future Earth observation constellation. Released from Tianzhou 1 2017 Aug 1, possibly as a test of a cubesat deployment mechanism for use on a space station.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 2, 21:35	6769	0.0007	387	395	92.37	42.79	226
CZ 7 upper stage 2017-021B 42685						Re-entered - 2017 May 18 Life 28 days
Launched Tianzhou 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Apr 20, 18:40	6663	0.0131	198	372	90.21	42.78	172

2017-022 Falcon 9 v1.2 Kennedy Space Center						2017 May 1, 11:15
USA 276 2017-022A 42689						in space
Military technology satellite, possibly testing sensors for monitoring other objects in orbit. Orbit at similar height to ISS and passed withing 5km of ISS 2017 Jun 3. Orbit information based on amateur observations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 24, 10:49	6777	0.0014	389	408	92.54	50.00	91
2017 Jun 2, 19:48	6777	0.0017	387	410	92.53	50.01	121
2018 Jul 10, 23:07	6771	0.0010	386	400	92.41	50.00	65
2018 Jul 11, 22:12	6772	0.0010	387	401	92.44	50.00	74
Falcon 9 upper stage uncatalogued						Re-entered - 2017 May 1 Life <1 day
Launched USA 276. Caused to re-enter about 4 hrs, 2.5 circuits, after launch above the southern Indian Ocean.
Not Catalogued - orbit parameters unavailable

2017-023 Ariane 5ECA (VA-236) Centre Spatiale Guyanaise						2017 May 4, 21:50
Mugunghwa 7 (Koreasat 7) 2017-023A 42691						in space
South Korean communications satellite covering Korea, the Philippines, the Indochinese Peninsula, India and Indonesia. It provides a range of video and data applications, including Internet access, direct-to-home broadcasting (DTH), government communications and connectivity for VSAT (Very Small Aperture Terminal) networks. Separated from the launch vehicle at 22:26 UTC. Expected location 116° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 May 5, 18:32	24391	0.7279	260	35766	631.83	4.01	179
2017 May 7, 08:59	27332	0.5414	6155	35752	749.47	2.16	178
2017 May 9, 14:25	42032	0.0027	35542	35766	1429.33	0.05	114	110°.0 E
2017 May 12, 23:16	42117	0.0012	35687	35792	1433.67	0.05	63	114°.5 E
2017 May 15, 21:01	42165	0.0001	35784	35789	1436.11	0.06	32	114°.5 E
2023 Feb 13, 00:53	42164	0.0001	35782	35789	1436.05	0.03	348	115°.9 E
SGDC (Geostationary Satellite for Communications and Defense) 2017-023B 42692						in space
Brazilian government satellite providing high-quality Internet services as part of the National Broadband Plan, and offering secure strategic communications links for the Brazilian Government. Separated from the launch vehicle at 22:18 UTC. Expected location 75° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 May 5, 18:45	24379	0.7277	260	35742	631.37	4.01	179
2017 May 8, 14:08	36158	0.1646	23829	35730	1140.42	0.44	176
2017 May 9, 22:58	42044	0.0021	35576	35756	1429.93	0.03	190	79°.0 W
2017 May 12, 13:52	42055	0.0018	35602	35752	1430.50	0.07	91	74°.8 W
2017 May 12, 21:47	42115	0.0007	35708	35766	1433.55	0.05	55	74°.5 W
2017 May 16, 11:27	42165	0.0000	35786	35788	1436.12	0.06	342	74°.3 W
2023 Feb 11, 19:32	42164	0.0002	35777	35795	1436.08	0.01	242	74°.9 W
Ariane 5 upper stage 2017-023C 42693						in space
Launched Koreasat 7 and SGDC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 5, 18:36	24414	0.7279	265	35807	632.74	4.07	181

2017-024 GSLV Mk II F09 Satish Dhawan Space Centre						2017 May 5, 11:27
GSat 9 (South Asia Satellite) 2017-024A 42695						in space
Indian communications satellite offering a range of communications services to India and members of the South Asian Association for Regional Cooperation (SAARC) - Afghanistan, Bangladesh, Bhutan, the Maldives, Nepal, Sri Lanka. Also carries GAGAN (GPS Aided GEO Augmented Navigation) to augment IRNSS services across Asia Expected location 48° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 May 6, 18:55	24415	0.7337	124	35950	632.77	20.61	179
2017 May 9, 15:27	24322	0.7334	105	35782	629.14	20.57	181
2017 May 10, 22:38	42122	0.0028	35624	35864	1433.93	0.06	259	93°.4 E
2017 May 23, 14:41	42165	0.0004	35771	35803	1436.10	0.04	198	97°.3 E
2023 Feb 12, 14:10	42164	0.0002	35778	35795	1436.08	0.08	35	97°.3 E
GSLV third stage 2017-024B 42696						Re-entered - 2017 Oct 10 Life 158 days
Launched GSat 9.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 9, 15:28	24322	0.7327	122	35766	629.16	20.59	181

2017-025 Falcon 9 v1.2 Kennedy Space Center						2017 May 15, 23:21
Inmarsat 5-F4 (GX-4) 2017-025A 42698						in space
Communications satellite including support for Inmarsat@s Global Xpresss network internet and intranet use, video on demand, video-conferencing, fax, e-mail, telephone and high-speed LAN access. Expected location: 56°.5 east where it arrived eleven months after launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 May 16, 11:12	41492	0.8371	382	69845	1401.84	24.48	181
2017 May 23, 12:58	53613	0.4263	24381	70089	2059.04	1.48	186
2017 May 26, 21:35	45338	0.2401	28072	49847	1601.22	0.16	249
2017 May 31, 23:18	42168	0.1833	28061	43518	1436.25	0.21	323	83°.2 E
2017 Jun 5, 22:47	42196	0.1747	28447	43189	1437.68	0.20	323	83°.1 E
2017 Jul 18, 22:24	42104	0.0280	34548	36903	1432.98	0.11	326	84°.1 E
2017 Aug 7, 21:19	42164	0.0001	35784	35788	1436.07	0.07	335	83°.5 E
2017 Nov 12, 14:58	42165	0.0000	35785	35789	1436.12	0.02	62	83°.5 E
2017 Nov 15, 14:39	42071	0.0001	35690	35695	1431.30	0.02	41	85°.2 E
2017 Nov 17, 09:28	41976	0.0000	35597	35599	1426.47	0.03	152
2017 Nov 28, 14:00	42024	0.0009	35607	35685	1428.92	0.03	56	115°.7 E
2017 Dec 1, 20:27	42165	0.0002	35780	35793	1436.10	0.04	194	117°.5 E
2018 Mar 17, 04:31	42165	0.0000	35787	35787	1436.12	0.06	349	117°.5 E
2018 Mar 19, 04:32	42309	0.0007	35903	35958	1443.45	0.06	64
2018 Apr 13, 06:28	42334	0.0001	35950	35961	1444.74	0.01	215
2018 Apr 14, 06:33	42309	0.0011	35884	35978	1443.48	0.00	233
2018 Apr 16, 06:34	42206	0.0006	35801	35854	1438.19	0.00	187	57°.0 E
2018 Apr 17, 06:32	42165	0.0000	35785	35789	1436.11	0.02	58	56°.5 E
2023 Feb 12, 18:26	42165	0.0001	35784	35789	1436.10	0.02	227	56°.5 E
Falcon 9 upper stage 2017-025B 42699						Re-entered - 2022 May 11 Life 1822 days
Launched Inmarsat 5-F4.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 25, 04:37	41487	0.8372	376	69842	1401.63	24.58	183

2017-I09 Nanoracks Cubesat Deployer International Space Station						2017 May 16, 08:25
Havelsat 1998-067LH 42700						Re-entered - 2019 Feb 28 Life 653 days
2U Cubesat developed by HAVELSAN, a Turkish IT company, and Istanbul Technical University carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 18:56	6780	0.0006	398	406	92.60	51.64	225
SOMP 2 (Students' Oxygen Measurement Project) 1998-067LJ 42701						Re-entered - 2019 Mar 19 Life 672 days
2U Cubesat with a payload to test a flexible TFSC (Thin Film Solar Cells) array. Also carries an amateur radio payload and instruments to carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 21:33	6780	0.0005	399	406	92.60	51.64	238
Columbia Sat 1998-067LK 42702						Re-entered - 2018 Mar 7 Life 295 days
2U Cubesat developed by the University of Michigan and built by the Universidad del Turabo, Gurabo, Puerto Rico carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 18:57	6780	0.0007	397	406	92.60	51.64	215

2017-I10 Nanoracks Cubesat Deployer International Space Station						2017 May 16, 11:55
KySat 3 1998-067LL 42703						Re-entered - 2018 May 7 Life 356 days
1U Cubesat with hardware and software designed, built, and tested by students of the University of Kentucky. Carries a stellar gyroscope to measure orientation by referring to the fixed star background, and a passive magnetic orientation system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 21:34	6780	0.0003	400	404	92.61	51.64	166
CXBN 2 (Cosmic X-ray Background Nanosatellite) 1998-067LM 42704						Re-entered - 2019 Mar 1 Life 654 days
2U Cubesat from Morehead State University,Kentucky using a new type of Cadmium Zinc Telluride detector to map the extragalactic diffuse cosmis x-ray background radiation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 21:34	6781	0.0002	401	404	92.61	51.64	134
IceCube 1998-067LN 42705						Re-entered - 2018 Oct 3 Life 505 days
3U Cubesat, a NASA Goddard Space Flight Center mission to validate a new 874 GHz submillimeter wave radiometer for cloud ice observations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 21:35	6781	0.0004	400	405	92.61	51.64	173

2017-I11 Nanoracks Cubesat Deployer International Space Station						2017 May 17, 01:45
Phoenix 1998-067LP 42706						Re-entered - 2019 May 8 Life 721 days
2U Cubesat from the National Cheng Kung University, Taiwan carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 21:34	6780	0.0001	402	403	92.60	51.64	203
X-Cubesat 1998-067LQ 42707						Re-entered - 2019 Feb 4 Life 628 days
2U Cubesat designed by students from the French École Polytechnique carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 21:34	6780	0.0001	401	403	92.61	51.64	194
qbee50-LTU-OC 1998-067LR 42708						Re-entered - 2019 Feb 26 Life 650 days
2U Cubesat from Luleå University of Technology, Sweden carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 21:34	6780	0.0001	401	403	92.61	51.64	181

2017-I12 Nanoracks Cubesat Deployer International Space Station						2017 May 17, 08:13
Altair 1 (Altair Pathfinder) 1998-067LS 42711						Re-entered - 2019 Dec 8 Life 935 days
6U Cubesat (6x1) from NASA to test and space qualify new technologies developed by Millennium Space Systems of El Segundo, California, including a new class of navigation sensors and demonstration of on board processing for next generation radios.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 12:04	6781	0.0002	401	404	92.62	51.64	155

2017-I13 Nanoracks Cubesat Deployer International Space Station						2017 May 17, 12:40
SHARC (Spacecraft for High Accuracy Radar Calibration) 1998-067LT 42712						Re-entered - 2019 May 4 Life 717 days
5U Cubesat from the US Air Force Research Laboratory (AFRL). Used as a callibration target for US Department of Defense C-band radar installations by comparing the satellite's onboard orbit measurements with ground -based radar measurements using a trransponder on the satellite, and laser ranging measurements. The onboard GPS orbit measurement system from the University of New South Wales (UNSW), Sydney and Australia's Defence Science and Technology (DST) Group is conducting a range of experiments aimed at increasing the understanding of outer atmospheric effects on small satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 19, 10:34	6782	0.0005	400	407	92.63	51.64	151

2017-I14 Nanoracks Cubesat Deployer International Space Station						2017 May 18, 01:00
ZA-Aerosat 1998-067LU 42713						Re-entered - 2019 Jun 2 Life 745 days
2U Cubesat from Stellenbosch University, South Africa carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 21:35	6781	0.0003	401	405	92.61	51.64	158
LINK (Little Intelligent Nanosatellite of KAIST) 1998-067LV 42714						Re-entered - 2018 Sep 23 Life 493 days
2U Cubesat from the Korea Advanced Institute of Science & Technology (South Korea) carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 12:04	6781	0.0002	401	404	92.62	51.64	149

2017-I15 Nanoracks Cubesat Deployer International Space Station						2017 May 18, 04:15
CSUNSaT 1 1998-067LW 42715						Re-entered - 2019 May 5 Life 717 days
2U Cubesat from California State University and NASA/JPL testing a new light-weight, longe-life battery designed for use in space.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 21:36	6781	0.0003	401	405	92.62	51.64	139

2017-I16 Nanoracks Cubesat Deployer International Space Station						2017 May 18, 08:25
UPSat 1998-067LX 42716						Re-entered - 2018 Nov 12 Life 543 days
2U Cubesat frome Libre Space Foundation & University of Patras, Greeece carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 22, 12:29	6781	0.0003	401	405	92.62	51.64	159
Spacecube 1998-067LY 42717						Re-entered - 2019 Mar 1 Life 652 days
2U Cubesat from France's École des Mines carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 23, 08:42	6781	0.0003	400	405	92.61	51.64	237
2017 May 25, 11:38	6781	0.0002	401	404	92.61	51.64	240
HOOPOE 1998-067LZ 42718						Re-entered - 2018 Dec 22 Life 583 days
2U Cubesat from the Herzliya Science Center, Israel carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 25, 11:01	6780	0.0004	400	405	92.61	51.64	245

2017-026 Soyuz ST-A + Fregat-M (VS-17) Centre Spatiale Guyanaise						2017 May 18, 11:54
SES 15 2017-026A 42709						in space
Comsat. serving North America, Latin America and the Caribbean and providing high speed connections to government, VSAT networks and maritime customers. Expected location 129° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jun 11, 13:05	24982	0.5986	3649	33558	654.93	4.79	191
2017 Aug 22, 12:35	35613	0.4194	14299	44170	1114.73	2.16	217
2017 Sep 21, 20:29	38508	0.2864	21101	43159	1253.40	1.35	227
2017 Oct 25, 02:07	40764	0.1221	29410	39362	1365.14	0.62	235
2017 Nov 11, 12:55	41611	0.0328	33866	36599	1407.90	0.14	237
2017 Nov 14, 07:47	41876	0.0151	34868	36128	1421.39	0.04	191
2017 Nov 20, 05:10	42165	0.0001	35785	35789	1436.11	0.02	155	137°.0 W
2017 Dec 17, 03:24	42165	0.0001	35781	35793	1436.12	0.06	287	136°.9 W
2017 Dec 22, 02:35	42122	0.0009	35705	35781	1433.89	0.05	323	129°.6 W
2023 Feb 12, 12:22	42165	0.0000	35786	35788	1436.12	0.03	0	129°.2 W
Fregat rocket stage 2017-026B 42710						in space
Launched SES 15.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 21, 18:11	23216	0.6240	2351	31324	586.71	6.15	179

2017-F02 - failed to reach orbit Electron (Its a Test) Rocket Lab Launch Complex, New Zealand						2017 May 25, 04:20
Dummy payload?
First test flight of Rocket Labs Electron launch vehicle. Failed when a fault in an item of ground equipment caused telemetry to be lost during second stage flight so the self destruct mechanism was triggered.

2017-I17 Nanoracks Cubesat Deployer International Space Station						2017 May 25, 05:25
Challenger Sat 1998-067MA 42721						Re-entered - 2018 Aug 12 Life 444 days
2U Cubesat the University of Colorado Boulder carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 30, 11:52	6781	0.0007	398	407	92.61	51.64	245
NjUST 1 1998-067MB 42722						Re-entered - 2019 Jul 20 Life 786 days
2U Cubesat from Nanjin University of Science and Technology carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 30, 11:52	6781	0.0007	398	408	92.62	51.64	240
UNSW-EC0 1998-067MC 42723						Re-entered - 2018 Dec 3 Life 557 days
2U Cubesat from the University of New South Wales carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 30, 21:02	6781	0.0007	398	407	92.61	51.64	239

2017-027 Soyuz-2.1b + Fregat Plesetsk Cosmodrome						2017 May 25, 06:33
Cosmos 2518 (EKS 2/Tundra 12L) 2017-027A 42719						in space
Missile early warning satellite capable of tracking missiles and other heat sources in the Earth's atmosphere and in space. May also carry a strategic communications system for use by the Russian Military. Reached operational orbit Dec 10.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 1, 06:32	26461	0.6964	1656	38509	713.93	63.81	270
2017 Jun 2, 00:14	26500	0.6968	1656	38588	715.52	63.81	270
2017 Jun 7, 16:01	26550	0.6973	1659	38685	717.55	63.80	270
Fregat rocket stage 2017-027B 42720						in space
Launched Cosmos 2518.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 28, 07:34	26442	0.6958	1665	38463	713.18	63.89	270

2017-I18 Nanoracks Cubesat Deployer International Space Station						2017 May 25, 08:34
DUThSat 1998-067MD 42724						Re-entered - 2018 Aug 26 Life 458 days
2U Cubesat from the Electromagnetic Theory Laboratory of the Democritus University of Thrace carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 31, 21:23	6781	0.0006	399	407	92.61	51.64	250
Lilacsat 1 1998-067ME 42725						Re-entered - 2019 Mar 28 Life 672 days
2U Cubesat. from the Harbin Institute of Technology, China carrying an amateur radio package and instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 28, 10:05	6781	0.0006	399	407	92.63	51.64	237
nSight 1 1998-067MF 42726						Re-entered - 2020 Apr 25 Life 1066 days
2U Cubesat from SCS Aerospace Group of Cape Town South Africa carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 31, 21:24	6781	0.0006	399	407	92.62	51.64	250

2017-I19 Nanoracks Cubesat Deployer International Space Station						2017 May 25, 11:55
QBITO 1998-067MH 42728						Re-entered - 2019 Feb 16 Life 632 days
2U Cubesat developed by students and faculty of the Universidad Politécnica de Madrid, Spain carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 28, 11:38	6781	0.0003	401	405	92.62	51.64	247
Aalto 2 1998-067MJ 42729						Re-entered - 2019 Feb 6 Life 622 days
2U Cubesat from Aalto University, Finland carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 30, 21:03	6781	0.0005	399	406	92.62	51.64	243
SuSat 1998-067MK 42730						Re-entered - 2019 Mar 21 Life 665 days
2U Cubesat from the University of Adelaide, Australia carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 31, 04:25	6781	0.0003	401	405	92.62	51.64	256

2017-I20 Nanoracks Cubesat Deployer International Space Station						2017 May 25, 23:40
SNUSaT 1A 1998-067MG 42727						Re-entered - 2019 Mar 31 Life 675 days
2U Cubesat from Seoul National University, Korea, one of a simultaneously-launched pair carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 26, 12:25	6782	0.0008	398	409	92.63	51.64	189

2017-I21 Nanoracks Cubesat Deployer International Space Station						2017 May 26, 04:00
INSPIRE 2 1998-067ML 42731						Re-entered - 2018 Nov 24 Life 547 days
2U Cubesat from University of Sydney, Australia carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 28, 13:11	6781	0.0007	398	408	92.62	51.64	179
PolyITAN-2-SAU 1998-067MM 42732						Re-entered - 2019 Feb 5 Life 620 days
2U Cubesat from the National Technical University, Ukraine carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission. Operation until 2019 Feb 5.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 28, 11:38	6781	0.0007	398	408	92.62	51.64	178
SNUSaT-1B 1998-067MN 42733						Re-entered - 2019 Mar 14 Life 657 days
2U Cubesat from Seoul National University, Korea, one of a simultaneously-launched pair carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 2, 19:40	6781	0.0007	398	407	92.61	51.64	200

2017-I22 Nanoracks Cubesat Deployer International Space Station						2017 May 26, 08:55
ExAlta 1 1998-067MP 42734						Re-entered - 2018 Nov 14 Life 537 days
2U Cubesat from the University of Alberta carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 27, 02:14	6781	0.0009	397	409	92.62	51.64	200

2017-I23 Nanoracks Cubesat Deployer International Space Station						2017 May 26, 21:15
Aoxiang 1 1998-067MQ 42735						Re-entered - 2019 Jun 26 Life 761 days
2U Cubesat from Northwestern Polytechnical University, China. carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 31, 04:26	6781	0.0008	397	408	92.61	51.64	240
BeEagleSat 1998-067MR 42736						Re-entered - 2019 Apr 27 Life 701 days
2U Cubesat from the Istanbul Technical University and HALVESAN (a turkish company) carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 30, 10:17	6781	0.0007	398	408	92.61	51.64	249
Atlantis Sat 1998-067MS 42737						Re-entered - 2018 Mar 28 Life 306 days
2U Cubesat from the University of Michigan Space Physics Research Laboratory carrying instruments to measure the behaviour of the lower thermosphere as part of the QB50 mission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 May 31, 21:24	6780	0.0007	397	407	92.61	51.64	240

2017-028 H-IIA 202 (F-34) Tanegashima Space Centre						2017 Jun 1, 00:17
Michibiki 2 (QZSS 2) 2017-028A 42738						in space
Quasi Zenith Satellite System satellite providing a timing and positioning service to improve navigational accuracy for users in Japan from a combination of equatorial GEO and inclined GEO, giving coverage to areas where the topography works against GPS reception. “Michibiki" translates into English as "Showing the Way".
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jun 1, 21:57	27917	0.5177	7087	35990	773.67	38.75	181
2017 Jun 2, 18:17	29335	0.4446	9916	35998	833.36	39.93	182
2017 Jun 6, 08:41	42329	0.0010	35910	35991	1444.49	44.78	137
2017 Jun 11, 16:14	42182	0.0751	32637	38971	1436.99	44.79	270	137°.3 E
2017 Jun 26, 15:29	42169	0.0753	32617	38965	1436.33	44.74	270	136°.3 E
2017 Jul 17, 09:35	42147	0.0752	32601	38937	1435.20	44.74	270	137°.5 E
2017 Jul 18, 20:17	42165	0.0747	32636	38937	1436.09	44.74	270	137°.7 E
H-IIA upper stage 2017-028B 42739						in space
Launched Michibiki 2.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 4, 06:46	24252	0.7252	286	35461	626.42	31.82	182

2017-029 Ariane 5ECA (VA-237) Centre Spatiale Guyanaise						2017 Jun 1, 23:45
Viasat 2 2017-029A 42740						in space
Commercial comsat providing broadband services to North America for the aviation industry, government and private consumers. Performance was lower than expected because of defects in two of its aerials. Expected location 69°.9 west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jun 4, 06:10	24391	0.7275	268	35758	631.84	6.07	181
2017 Jun 5, 18:01	26030	0.7445	272	39031	696.57	6.01	181
2017 Jun 6, 17:33	28032	0.7625	279	43029	778.48	5.99	181
2017 Jun 9, 15:10	33742	0.8020	303	54425	1028.07	5.96	182
2017 Jun 13, 11:06	39177	0.5525	11155	54442	1286.18	0.63	199
2017 Jun 14, 21:37	41791	0.4556	16374	54452	1417.05	0.32	333
2017 Jun 22, 03:07	42041	0.4470	16871	54455	1429.78	0.38	340	91°.1 W
2017 Aug 16, 05:49	42163	0.3025	23029	48542	1436.03	0.24	340	87°.2 W
2017 Sep 19, 03:50	42251	0.2118	26926	44820	1440.52	0.16	340
2017 Nov 30, 23:59	42164	0.0000	35785	35787	1436.06	0.02	256	69°.9 W
2023 Feb 12, 19:33	42165	0.0000	35786	35787	1436.10	0.04	162	69°.9 W
Eutelsat 172B 2017-029B 42741						in space
Comsat offering trans-Pacific services and services to the North Pacific, North East Asia, South East Pacific, South West Pacific and South Pacific areas as well broadband services to aviation. Expected location 172° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jun 9, 16:56	24595	0.7194	524	35910	639.79	5.89	184
2017 Jun 16, 13:46	25763	0.6978	1408	37362	685.89	5.22	189
2017 Jul 17, 10:32	32493	0.5839	7143	45087	971.52	3.21	208
2017 Aug 10, 07:59	36981	0.4544	13797	47409	1179.59	1.97	218
2017 Sep 6, 01:12	39397	0.2518	23099	42939	1297.05	1.05	225
2017 Oct 12, 10:51	42165	0.0001	35782	35792	1436.12	0.06	278	176°.0 E
2017 Nov 16, 08:38	42249	0.0004	35855	35887	1440.41	0.01	182
2017 Nov 20, 16:24	42165	0.0001	35783	35791	1436.11	0.04	170	172°.1 E
2023 Feb 12, 20:42	42165	0.0000	35785	35788	1436.10	0.05	298	172°.0 E
Ariane 5 upper stage 2017-029C 42742						in space
Launched Viasat 2 and Intelsat 172B.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 3, 18:41	24475	0.7208	456	35736	635.08	5.89	180

2017-030 Falcon 9 v1.2 Kennedy Space Center						2017 Jun 3, 21:07
SpaceX Dragon CRS-11 2017-030A 42744						Re-entered - 2017 Jul 3 Life 30 days Returned to Earth
Carrying a cargo to the ISS under NASA's Commercial Resupply Services (CRS) contract. Captured by the ISS Remote Manipulator System Jun 5 at 13:52 UTC and attached to the lower port of the Harmony module at 16:07 UTC. Undocked using the RMS 2017 Jul 3 at about 18:00 UTC. Released Jul 3 at 06:41 UTC after a one day delay due to weather in the splashdown area. Retro-fire led to splashdown at 12:12 UTC in the Pacific Ocean, about 300 km SW of Baja, California.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jun 3, 23:01	6658	0.0113	204	355	90.11	51.64	45
2017 Jun 4, 02:02	6661	0.0117	205	361	90.17	51.64	47
2017 Jun 4, 06:43	6659	0.0113	205	356	90.13	51.66	47
2017 Jun 5, 08:34	6783	0.0005	402	408	92.67	51.64	235
Falcon 9 upper stage uncatalogued						Re-entered - 2017 Jun 3 Life <1 day
Launched SpaceX Dragon CRS-11. Caused to re-enter before it could be catalogued.
Not Catalogued - orbit parameters unavailable

2017-031 GSLV Mk III D1 Satish Dhawan Space Centre						2017 Jun 5, 11:58
GSat 19 2017-031A 42747						in space
Indian communications satellite. Also fitted with GRASP (Geostationary Radiation Spectrometer) to monitor chrged particles and monitor their influence on electronic components. Expected location - 48° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jun 6, 13:35	23737	0.7251	148	34571	606.61	21.67	179
2017 Jun 10, 01:36	39421	0.0722	30198	35887	1298.21	0.77	182
2017 Jun 14, 19:45	42062	0.0052	35463	35905	1430.86	0.10	273	82°.4 E
2017 Jun 21, 23:04	42165	0.0003	35774	35799	1436.11	0.06	173	82°.5 E
2018 Jan 4, 11:37	42221	0.0001	35837	35848	1438.96	0.06	216	81°.6 E
2018 Jan 5, 11:38	42244	0.0001	35860	35871	1440.14	0.02	359
2018 Feb 9, 11:30	42163	0.0003	35773	35798	1436.03	0.01	221	47°.9 E
2023 Feb 12, 18:23	42165	0.0004	35771	35802	1436.09	0.06	117	47°.9 E
GSLV third stage 2017-031B 42748						Re-entered - 2018 Feb 8 Life 248 days
Mission information in preparation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 12, 00:28	23724	0.7245	158	34534	606.09	21.74	183

2017-032 Proton-M + Briz-M Baikonur Cosmodrome						2017 Jun 8, 03:45
Echostar 21 2017-032A 42749						in space
European communications satellite operated by Echostar Corporation providing services to continental Europe. The satellite was originally built as a ground spare for TerreStar networks. Expected location - 10°.25 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jun 8, 23:12	25392	0.6615	2217	35811	671.14	30.66	0
2017 Jun 13, 11:11	36543	0.1543	24526	35804	1158.70	9.89	1
2017 Jun 22, 08:37	42165	0.0002	35779	35795	1436.12	7.48	344	10°.3 E
2023 Feb 12, 18:12	42164	0.0002	35777	35795	1436.07	3.48	15	10°.3 E
Briz-M rocket stage 2017-032B 42750						in space
Launched Echostar 21.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 8, 11:52	12535	0.4654	323	11990	232.78	49.74	352
2017 Jun 12, 07:06	24501	0.6664	1795	34452	636.13	31.15	3

2017-033 Soyuz-2.1a Baikonur Cosmodrome						2017 Jun 14, 09:20
Progress MS-06 (Progress 7K-MS №436) 2017-033A 42756						Re-entered - 2017 Dec 28 Life 197 days
Supplies to ISS. Docked with the aft port of Zvezda 2017 Jun 16 at 11:37 UTC. Undocked 2017 Dec 28 at 01:03:30 UTC. Retrofire at 04:10 UTC resulted in a destructive re-entry at 04:43 UTC with any surviving fragments impacting the southern Pacific Ocean at around 04:51 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 14, 15:25	6690	0.0014	303	321	90.76	51.64	241
2017 Jun 16, 11:00	6783	0.0004	402	408	92.66	51.64	283
Soyuz upper stage 2017-033B 42757						Re-entered - 2017 Jun 17 Life 3 days
Launched Progress MS-06.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 14, 15:25	6580	0.0024	186	218	88.54	51.64	68

2017-034 CZ 4B Jiuquan Space Centre						2017 Jun 15, 03:00
HXMT (Hard X-ray Modulation Telescope) 2017-034A 42758						in space
X-Ray and Gamma-ray astronomical observatory.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 15, 19:14	6919	0.0006	537	545	95.47	43.02	345
2017 Jun 22, 11:32	6921	0.0007	538	547	95.49	43.02	28
Zhuhai-1 OVS-01A 2017-034B 42759						in space
Prototype commercial Chinese remote sensing satellite using high definition video. From Zhuhai Orbita Aerospace Science and Technology Co. Providing data services for agriculture, land and water resources, environmental protection and transport.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 15, 17:03	6918	0.0008	534	545	95.43	43.02	330
ÑuSat 03 (Milanesat) 2017-034C 42760						in space
Small satellite from Satellogic of Argentina providing earth images in the visible and infrared parts of the spectrum using real-time imaging and video.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 15, 19:11	6918	0.0007	536	545	95.45	43.02	338
Zhuhai-1 OVS-01B 2017-034D 42761						in space
Demonstration version of commercial Chinese remote sensing satellite using high definition video. From Zhuhai Orbita Aerospace Science and Technology Co. Providing data services for agriculture, land and water resources, environmental protection and transport.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 15, 19:14	6918	0.0008	534	545	95.43	43.02	332
CZ 4B third stage 2017-034E 42762						Re-entered - 2018 Aug 25 Life 436 days
Launched HXMT and other satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 16, 14:07	6783	0.0202	268	542	92.66	43.12	5

2017-035 CZ 3B Xichang Space Centre						2017 Jun 18, 16:11
Zhongxing 9A (Chinasat 9A) 2017-035A 42763						in space
Chinese communications satellite. Abnormal operation of launch vehicle stage 3 resulted in a lower than expected tranfer orbit. More time than usual was needed to reach its geosynchronous slot where it arrived 2017 Jul 5. Planned for 15 years operational life but having used station-keeping propellant to correct launch vehicle under-performance, it was moved to graveyard orbit 2021 Feb. Expected location 101°.4 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jun 19, 07:18	15049	0.5595	251	17090	306.20	26.82	185
2017 Jul 7, 23:08	42164	0.0003	35774	35798	1436.06	0.05	212	101°.4 E
2021 Feb 5, 12:36	42167	0.0001	35782	35795	1436.19	0.03	89	101°.2 E
2021 Feb 12, 09:33	42173	0.0003	35784	35806	1436.54	0.04	115	100°.8 E
2021 Feb 23, 12:31	42300	0.0007	35894	35951	1443.03	0.02	245
2023 Feb 13, 02:34	42303	0.0005	35902	35948	1443.18	1.83	275
CZ 3B fourth stage 2017-035B 42764						Re-entered - 2022 Jan 2 Life 1659 days
Launched Chinasat 9A.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 19, 04:52	14651	0.5515	192	16354	294.15	25.68	179

2017-036 PSLV-XL (PSLV C-38) Satish Dhawan Space Centre						2017 Jun 23, 03:59
UCLsat 2017-036A 42765						Re-entered - 2023 Nov 19 Life 2340 days
2U Cubesat from the University College of London as part of the QB50 project. Equipped with sensors to monitor radiation and charged particles in the space environment.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 23, 17:07	6719	0.0009	334	347	91.35	97.01	282
NIUSat 2017-036B 42766						Re-entered - 2024 Apr 27 Life 2500 days
Satellite from Noorul Isalm University, built to provide multispectral imagery for agricultural crop monitoring and disaster management support applications.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 23, 22:18	6886	0.0015	497	518	94.77	97.45	232
2023 Feb 13, 13:06	6847	0.0012	461	477	93.98	97.18	179
Cartosat 2E 2017-036C 42767						in space
Indian remote sensing satellite to collect high-resolution large-scale imagery for use in urban planning, infrastructure development, utilities planning, and traffic management.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Jun 23, 22:18	6886	0.0015	497	518	94.78	97.45	232	09:29
2023 Feb 13, 07:45	6886	0.0007	503	513	94.79	97.42	263	09:32
LituanicaSat 2 2017-036D 42768						Re-entered - 2023 Apr 4 Life 2111 days
3U Cubesat from Lithuania built as a technology demonstrator, particularly a thruster system, as part of the QB50 programme.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 22:01	6886	0.0015	497	518	94.77	97.45	232
2023 Feb 13, 01:49	6760	0.0007	377	386	92.18	97.17	148
CE-Sat 1 (Canon Electric Satellite 1) 2017-036E 42769						in space
Small remote sensing satellite built by Canon Electronics.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 22:00	6885	0.0015	497	517	94.76	97.45	230
InflateSail 2017-036F 42770						Re-entered - 2017 Sep 3 Life 72 days
3U CubeSat with a 1 m long inflatable rigidizable mast, and a 10 sq metre sail to accelerate orbit decay.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 18:51	6885	0.0015	496	517	94.75	97.45	234
Lemur-2 (ShainaJohl) 2017-036G 42771						Re-entered - 2023 Sep 8 Life 2268 days
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and other sensors. Lemur-2 satellites are named after development and support team members. One of a cluster of eight similar satellites carried on this launch, 2017-036. To avoid clutter, the others are not listed separately. All satellites are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 30, 21:49	6885	0.0015	497	517	94.76	97.45	208
2023 Feb 13, 02:31	6819	0.0010	434	447	93.40	97.17	163
AALTO 1 2017-036L 42775						Re-entered - 2024 Sep 1 Life 2627 days
3U Cubesat created by students of Aalto University. Equipped with a spectrometer for Earth observation and a radiation monitoring payload. It also carries a small sail to accelerate the de-orbit process.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 22:00	6884	0.0013	497	515	94.74	97.45	229
2023 Feb 13, 07:37	6853	0.0011	467	483	94.10	97.17	181
URSa MAIOr (University of Rome la Sapienza Micro Attitude In Orbit testing) 2017-036M 42776						Re-entered - 2024 Jul 1 Life 2565 days
3U Cubesat from the University of Rome. Monitoring electron density and testing a thruster. Also carries a de-orbit sail to accelerate re-entry at mission end.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 20:25	6884	0.0013	497	515	94.74	97.45	230
2023 Feb 13, 08:57	6850	0.0011	464	479	94.03	97.17	178
COMPASS 2 (Complex Orbital Magneto-Plasma Autonomous Small Satellite 2) 2017-036N 42777						Re-entered - 2023 Jun 24 Life 2192 days
3U Cubesat from Russia equipped with an array of flexible solat cells and a drag sail. Part of the QB50 project.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:59	6883	0.0012	497	514	94.73	97.45	234
2023 Feb 12, 20:29	6803	0.0008	419	430	93.06	97.17	155
Max Valier Sat 2017-036P 42778						Re-entered - 2024 Jun 30 Life 2564 days
Small satellite named after the Max Valier technical high school, South Tyrol, Italy where the project was initiated. Carries a miniaturised X-ray telescope, a GPS receiver, an imaging system and an AIS receiver for messages transmitted by ships at sea.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:59	6883	0.0012	497	513	94.72	97.45	235
2023 Feb 13, 09:05	6846	0.0010	461	474	93.95	97.18	177
Diamond Red 2017-036U 42783						Re-entered - 2024 Apr 26 Life 2499 days
3U Cubesat - one of three simultaneously-launched demonstration satellites for a planned constellation of 200 vehicles that will provide narrow band comms links to ground-based users.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 17:15	6882	0.0011	497	512	94.71	97.45	245
Pegasus 2017-036V 42784						Re-entered - 2024 Jan 9 Life 2391 days
2U Cubesat studying electrons in space and carrying a puled plasma thruster. Part of the QB50 project.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:59	6882	0.0011	497	512	94.70	97.45	244
Diamond Green 2017-036W 42785						Re-entered - 2024 Apr 11 Life 2484 days
3U Cubesat - one of three simultaneously-launched demonstration satellites for a planned constellation of 200 vehicles that will provide narrow band comms links to ground-based users.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:59	6882	0.0011	497	512	94.70	97.45	244
Diamond Blue 2017-036X 42786						Re-entered - 2024 Apr 23 Life 2496 days
3U Cubesat - one of three simultaneously-launched demonstration satellites for a planned constellation of 200 vehicles that will provide narrow band comms links to ground-based users.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:59	6882	0.0011	497	512	94.70	97.45	244
2023 Feb 13, 00:40	6843	0.0009	459	471	93.90	97.17	182
NUDTSat (National University of Defense Technology Satellite) 2017-036Y 42787						Re-entered - 2023 May 31 Life 2168 days
2U Cubesat from the USA studying electrons and neutrons in space. Part of the QB50 project.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:59	6882	0.0011	497	511	94.70	97.45	244
2023 Feb 12, 23:41	6794	0.0007	411	421	92.89	97.17	158
SUChai (Satellite of the University of Chile for Aerospace Investigation) 2017-036Z 42788						Re-entered - 2023 Oct 11 Life 2301 days
1U Cubesat from the University of Chile studying the ionosphere, built as an aid to teaching methods and processes for designing and building satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 17:14	6882	0.0011	497	511	94.70	97.45	249
2023 Feb 13, 01:35	6822	0.0008	438	449	93.45	97.17	166
SKCube 2017-036AA 42789						Re-entered - 2023 Nov 14 Life 2335 days
1U Cubesat from Slovakia built to gain hands on experience of satellite design and construction. Part of the QB50 project.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 17:14	6882	0.0011	497	511	94.70	97.45	246
VZLUSAT 1 2017-036AB 42790						Re-entered - 2023 Jun 6 Life 2174 days
3U Cubesat from the Czech Republic, carrying a miniaturised X-ray sensor.Part of the QB50 project.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:59	6882	0.0010	497	511	94.69	97.45	244
VENTA 1 2017-036AC 42791						Re-entered - 2024 Jan 9 Life 2391 days
Small satellite from Latvia carrying an AIS receiver to collect messages from ships at sea.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:58	6882	0.0010	497	511	94.69	97.45	245
Robusta 1B 2017-036AD 42792						Re-entered - 2023 Oct 17 Life 2307 days
1U Cubesat carrying an experiment to check the deterioration of electronic components based on bipolar transistors, when exposed to space radiation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:58	6882	0.0010	496	511	94.69	97.45	245
2023 Feb 13, 01:49	6823	0.0008	440	450	93.49	97.17	167
CICERO 6 (Community Initiative for Cellular Earth Remote Observation) 2017-036AE 42793						Re-entered - 2024 Jun 11 Life 2545 days
6U Cubesat (3x2) equipped to perform GPS and Galileo radio occultation observations by the Earth's atmosphere and undertake surface remote sensing by reflected navigation satellite signals.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:58	6881	0.0009	496	509	94.68	97.45	246
2023 Feb 13, 08:45	6846	0.0008	462	473	93.95	97.17	178
D-Sat (De-orbit Satellite) 2017-036AF 42794						in space
1U Cubesat carrying an experiment to check the deterioration of electronic components based on bipolar transistors, when exposed to space radiation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:58	6881	0.0008	497	508	94.67	97.45	243
2023 Feb 13, 10:47	6963	0.0120	502	668	96.37	97.46	358
PACSCISAT 2017-036AG 42795						Re-entered - 2023 Mar 14 Life 2090 days
3U Cubesat from Pacific Scientific Energetic Materials Company, LLC, built by Tyvak International. Purpose was to demonstrate the capability of rocket motors and initiators.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 21:58	6881	0.0008	497	508	94.67	97.45	243
2017 Jul 1, 13:25	6881	0.0009	497	509	94.67	97.45	215
PSLV upper stage 2017-036AH 42796						Re-entered - 2018 Jul 24 Life 396 days
Launched Cartosat 2E and numerous other small satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 25, 18:31	6882	0.0011	497	511	94.70	97.45	241

2017-037 Soyuz-2.1v + Volga Plesetsk Cosmodrome						2017 Jun 23, 18:04
Cosmos 2519 2017-037A 42798						Re-entered - 2021 Dec 23 Life 1644 days
Military satellite. Acted as a target for close proximity manoeuvres by Cosmos 2521.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Jun 23, 21:53	7040	0.0011	654	669	97.97	98.05	241	09:54
2017 Aug 23, 14:07	7037	0.0014	649	668	97.91	97.92	57	09:53
2017 Oct 30, 13:19	7037	0.0012	650	667	97.91	97.91	186	09:49
2017 Dec 13, 21:54	7037	0.0013	649	668	97.91	97.90	56	09:46
2017 Dec 14, 14:49	7030	0.0014	642	662	97.78	97.90	59	09:46
2018 Jun 26, 21:29	7030	0.0012	643	661	97.77	97.87	141	09:35
2018 Jun 27, 08:53	7025	0.0007	642	652	97.67	97.88	185	09:35
2018 Jun 27, 18:39	7022	0.0010	637	650	97.60	97.87	232	09:35
2018 Jun 28, 09:33	7017	0.0014	629	649	97.50	97.87	259	09:35
2018 Jun 28, 20:40	7010	0.0020	618	646	97.35	97.87	284	09:35
2018 Jun 30, 13:45	6995	0.0034	593	641	97.04	97.87	301	09:35
2018 Jul 1, 15:41	6981	0.0051	567	638	96.74	97.86	308	09:35
2018 Jul 3, 12:48	6966	0.0067	541	635	96.43	97.86	309	09:35
2018 Jul 4, 09:10	6958	0.0077	526	634	96.28	97.86	309	09:35
2018 Jul 4, 20:24	6951	0.0085	513	632	96.12	97.86	308	09:35
2018 Jul 6, 14:03	6937	0.0103	487	629	95.82	97.85	307	09:35
2018 Jul 7, 12:58	6922	0.0119	461	626	95.52	97.85	308	09:35
2018 Jul 9, 14:17	6908	0.0135	436	623	95.23	97.85	303	09:35
2018 Jul 10, 12:31	6893	0.0153	410	621	94.93	97.86	304	09:36
2018 Jul 12, 12:04	6880	0.0167	387	617	94.65	97.86	300	09:36
2018 Jul 13, 11:08	6866	0.0182	363	613	94.37	97.86	301	09:36
2018 Jul 15, 11:54	6852	0.0200	337	610	94.07	97.85	295	09:37
2018 Jul 16, 12:59	6837	0.0215	312	606	93.78	97.85	295	09:37
2018 Jul 18, 13:29	6853	0.0234	315	635	94.10	97.86	288	09:38
2018 Jul 19, 13:03	6869	0.0253	317	664	94.43	97.86	285	09:38
Cosmos 2521 2017-037D 42919						Re-entered - 2019 Sep 12 Life 811 days
Military satellite. Separated from Cosmos 2519 around 2017 Aug 23 then conducted close proximity manoeuvres using it as a target.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Aug 23, 22:17	7038	0.0014	650	670	97.93	97.92	60	09:53
2017 Aug 28, 14:58	7036	0.0014	648	668	97.90	97.92	44	09:53
2017 Sep 4, 18:23	7037	0.0013	650	668	97.91	97.91	20	09:52
2017 Oct 30, 18:12	7037	0.0012	651	667	97.91	97.91	185	09:49
2018 Feb 13, 21:18	7037	0.0011	651	666	97.91	97.88	208	09:42
2018 Feb 14, 10:51	7019	0.0032	619	664	97.54	97.92	231	09:42
2018 Feb 20, 19:16	7031	0.0009	646	659	97.78	97.89	182	09:42
2018 Mar 19, 20:13	7028	0.0016	639	661	97.72	97.89	107	09:41
2018 Mar 20, 10:53	7030	0.0015	642	662	97.77	97.89	107	09:41
2018 Apr 30, 20:33	6738	0.0014	350	369	91.73	97.91	162	09:52
2018 Jul 19, 19:51	6732	0.0012	346	362	91.61	97.90	223	10:38
2018 Jul 20, 21:38	6698	0.0041	293	348	90.93	97.90	91	10:39
2018 Nov 1, 21:06	6668	0.0027	272	308	90.32	97.89	56	11:51
2018 Nov 2, 21:14	6684	0.0005	302	309	90.63	97.89	27	11:52
2018 Dec 18, 21:44	6668	0.0005	287	293	90.32	97.89	186	12:24
2018 Dec 19, 17:22	6693	0.0003	313	317	90.83	97.88	167	12:25
Cosmos 2523 2017-037E 42986						in space
Military satellite - mission unknown. Separated from Cosmos 2521 on 2017 Oct 30, probably around 04:00 UTC. Perigee lowered immediately, then performed no further obvious manoeuvres.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Oct 31, 02:08	6987	0.0078	554	664	96.88	97.88	215	09:49
Volga rocket stage 2017-037B 42799						Re-entered - 2017 Jun 27 Life 4 days
Launched Cosmos 2519. Caused to re-enter after four days.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 05:16	7040	0.0012	654	670	97.98	98.05	233
Soyuz third stage 2017-037C 42800						Re-entered - 2020 Apr 20 Life 1032 days
Launched Cosmos 2519.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 23, 22:35	6845	0.0267	284	650	93.94	98.06	73

2017-038 Falcon 9 v1.2 Kennedy Space Center						2017 Jun 23, 19:10
Bulgariasat 1 2017-038A 42801						in space
Bulgarian comsat providing high definition and ultra-high-definition television, very-small-aperture terminal (VSAT) communications, satellite news gathering relays, and other communications services, primarily to the Balkan Peninsula and Central/Western Europe. expected location. expected location 1°.9 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jun 24, 06:30	39157	0.8321	196	65361	1285.18	23.95	179
2017 Jun 30, 17:58	42350	0.0010	35929	36015	1445.59	0.01	51
2017 Jul 3, 14:50	42208	0.0029	35709	35951	1438.32	0.06	137	1°.9 E
2017 Jul 10, 23:51	42165	0.0001	35782	35792	1436.10	0.05	216	1°.9 E
2023 Feb 12, 09:29	42165	0.0003	35776	35798	1436.10	0.01	225	1°.9 E
Falcon 9 upper stage 2017-038B 42802						Re-entered - 2017 Oct 27 Life 126 days
Mission information in preparation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 24, 17:02	39101	0.8320	193	65253	1282.45	23.95	179

2017-039 Falcon 9 v1.2 Vandenberg Air Force Base						2017 Jun 25, 20:25
Iridium 113 (Iridium Next) 2017-039A 42803						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 26, 21:42	6994	0.0012	608	625	97.02	86.66	232
Iridium 123 (Iridium Next) 2017-039B 42804						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 26, 21:42	6994	0.0012	607	625	97.02	86.67	234
Iridium 120 (Iridium Next) 2017-039C 42805						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 26, 21:42	6995	0.0013	607	626	97.03	86.67	235
Iridium 115 (Iridium Next) 2017-039D 42806						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 26, 21:42	6994	0.0013	607	625	97.02	86.67	231
Iridium 118 (Iridium Next) 2017-039E 42807						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 26, 21:42	6995	0.0008	611	622	97.04	86.66	238
Iridium 117 (Iridium Next) 2017-039F 42808						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 26, 21:42	6994	0.0013	606	625	97.01	86.67	227
Iridium 126 (Iridium Next) 2017-039G 42809						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 26, 21:42	6994	0.0010	609	623	97.01	86.67	231
Iridium 124 (Iridium Next) 2017-039H 42810						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 26, 21:42	6995	0.0012	608	625	97.03	86.67	234
Iridium 128 (Iridium Next) 2017-039J 42811						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 26, 21:42	6995	0.0011	609	625	97.04	86.67	238
Iridium 121 (Iridium Next) 2017-039K 42812						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 26, 21:42	6995	0.0011	609	625	97.04	86.67	235
Falcon 9 upper stage uncatalogued						Re-entered - 2017 Jun 25 Life <1 day
Launched cluster of Iridium satellite. De-orbited soon after releasing payloads. Not catalogued.
Not Catalogued - orbit parameters unavailable

2017-040 Ariane 5ECA (VA-238) Centre Spatiale Guyanaise						2017 Jun 28, 21:15
Hellas Sat 3 2017-040A 42814						in space
Communications satellite delivering Direct to Home TV services and telecoms to Europe, the Middle East and sub-Saharan Africa. Also carries Inmarsat's EAN (European Aviation Network) service to provide in-flight broadband services to air passengers. Expected location - 39° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jun 29, 18:05	24384	0.7284	245	35767	631.57	2.96	178
2017 Jun 30, 13:09	27628	0.5253	6736	35764	761.71	1.86	178
2017 Jul 3, 07:40	42038	0.0025	35557	35764	1429.65	0.01	84	28°.7 E
2017 Jul 7, 22:06	42115	0.0012	35686	35789	1433.57	0.05	45	34°.4 E
2017 Jul 10, 16:31	42165	0.0001	35784	35789	1436.10	0.04	168	34°.5 E
2017 Aug 3, 00:54	42126	0.0010	35705	35791	1434.12	0.01	251	34°.4 E
2017 Aug 4, 00:48	42086	0.0001	35703	35713	1432.09	0.02	201	35°.0 E
2017 Aug 8, 00:18	42136	0.0005	35738	35777	1434.61	0.03	246	38°.5 E
2017 Aug 10, 00:09	42165	0.0003	35774	35800	1436.12	0.03	12	39°.0 E
2023 Feb 13, 06:15	42165	0.0004	35768	35806	1436.12	0.05	329	39°.0 E
GSat 17 2017-040B 42815						in space
Indian communications satellite providing communications and data relay services to India, the Middle East and South Asia. Also carries a search and rescue receiver ro detect emergency signals. Expected location - 93¯.5 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jun 29, 17:02	24404	0.7283	251	35800	632.32	2.97	178
2017 Jun 30, 23:16	30925	0.3639	13293	35801	902.03	0.96	176
2017 Jul 3, 15:27	42010	0.0045	35444	35819	1428.18	0.11	20	87°.3 E
2017 Jul 4, 11:49	42035	0.0046	35464	35849	1429.46	0.11	27	88°.8 E
2017 Jul 7, 12:08	42049	0.0041	35497	35844	1430.17	0.11	31	93°.3 E
2017 Jul 8, 11:13	42106	0.0013	35671	35784	1433.08	0.10	311	93°.1 E
2017 Jul 13, 14:16	42166	0.0004	35769	35806	1436.15	0.09	346	93°.5 E
2023 Feb 12, 20:19	42165	0.0006	35763	35810	1436.09	0.05	187	93°.5 E
Ariane 5 upper stage (VA-238) 2017-040C 42816						in space
Launched HellasSat and GSat 17.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jun 29, 10:58	24422	0.7286	250	35837	633.03	2.90	174

2017-F03 - failed to reach orbit CZ 5 (Y2) Wenchang Space Centre						2017 Jul 2, 11:23
Shijian 18 (Practice 18)
Experimental communications satellite aimed at geosynchronous orbit. Lost when a first stage engine of the CZ-5 launch vehicle underperformed so the payload could not reach orbit.

2017-041 Falcon 9 v1.2 Kennedy Space Center						2017 Jul 5, 23:38
Intelsat 35e 2017-041A 42818						in space
High capacity comsat providing Direct to Home services in the Caribbean, as well as services for mobility and government applications in the Caribbean, trans-Europe to Africa and the African continent. Expected location - 34°.5 west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Jul 6, 23:14	27926	0.7614	284	42812	774.07	25.83	178
2017 Jul 8, 00:34	28723	0.7279	1436	43253	807.41	21.87	179
2017 Jul 9, 23:48	29462	0.6691	3371	42797	838.79	17.22	179
2017 Jul 10, 23:00	31863	0.5429	8187	42784	943.40	10.68	179
2017 Jul 18, 03:51	42710	0.0248	35274	37390	1464.04	0.13	329
2017 Jul 19, 12:16	42186	0.0008	35777	35840	1437.20	0.29	214	32°.9 W
2017 Jul 20, 16:54	42165	0.0002	35778	35795	1436.09	0.10	234	33°.0 W
2017 Aug 12, 04:50	42199	0.0002	35811	35830	1437.82	0.07	226	33°.4 W
2017 Aug 16, 04:39	42165	0.0003	35776	35798	1436.11	0.06	225	34°.5 W
2023 Feb 13, 04:19	42165	0.0002	35779	35794	1436.09	0.02	219	34°.5 W
Falcon 9 upper stage 2017-041B 42819						in space
Launched Intesat 35E.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 7, 08:32	27860	0.7609	284	42680	771.31	25.86	178

2017-I24 JEM Small Satellite Orbital Deployer International Space Station						2017 Jul 7, 08:50
TOKI 1998-067MU 42820						Re-entered - 2019 May 3 Life 665 days
1U Cubesat from Japan. One of five identical satellites built under the Birds-1 International programme supported by the Kyushu Institute of Technology, Japan. Each satellite is equipped with an imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 10, 04:24	6780	0.0002	401	403	92.60	51.64	341
Ghanasat 1 1998-067MV 42821						Re-entered - 2019 May 22 Life 684 days
1U Cubesat from Ghana. One of five identical satellites built under the Birds-1 International programme supported by the Kyushu Institute of Technology, Japan. Each satellite is equipped with an imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 9, 16:43	6781	0.0004	400	405	92.61	51.64	347
Mazaalai 1998-067MW 42822						Re-entered - 2019 May 11 Life 673 days
1U Cubesat from Mongolia. One of five identical satellites built under the Birds-1 International programme supported by the Kyushu Institute of Technology, Japan. Each satellite is equipped with an imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 9, 13:24	6781	0.0004	400	406	92.61	51.64	343

2017-I25 JEM Small Satellite Orbital Deployer International Space Station						2017 Jul 7, 09:10
BRAC Onnesha 1998-067MX 42823						Re-entered - 2019 May 6 Life 668 days
1U Cubesat from Bangladesh. One of five identical satellites built under the Birds-1 International programme supported by the Kyushu Institute of Technology, Japan. Each satellite is equipped with an imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 9, 13:34	6781	0.0008	398	408	92.62	51.64	355
Nigeria EduSat-1 1998-067MY 42824						Re-entered - 2019 May 13 Life 675 days
1U Cubesat from Nigeria. One of five identical satellites built under the Birds-1 International programme supported by the Kyushu Institute of Technology, Japan. Each satellite is equipped with an imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 9, 16:43	6781	0.0007	398	407	92.62	51.64	356

2017-042 Soyuz-2.1a + Fregat Baikonur Cosmodrome						2017 Jul 14, 06:36
Canopus-Vulcan 2 (Canopus-Vulcan IK) 2017-042A 42825						in space
Small Russian remote sensing satellite using visible and infrared wavelengths to detect sources of fire as small as five by five meters across a 2000 kilometer swath of land.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Jul 14, 19:35	6886	0.0003	506	510	94.77	97.44	88	23:30
2023 Feb 13, 09:38	6882	0.0002	502	505	94.69	97.42	86	23:25
NorSat 1 2017-042B 42826						in space
Small satellite from Norway investigating solar radiation and space weather. It also carries a receiver for AIS messages from ships at sea.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 19, 13:42	6975	0.0014	587	606	96.62	97.61	218
2023 Feb 13, 11:54	6966	0.0013	578	596	96.43	97.40	280
NorSat 2 2017-042D 42828						in space
Small satellite from Norway investigating solar radiation and space weather. It also carries a receiver for AIS messages from ships at sea.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 19, 13:41	6974	0.0013	587	605	96.60	97.62	221
2023 Feb 12, 20:06	6963	0.0012	576	593	96.37	97.40	280
TechnoSat (Tubsat 12) 2017-042E 42829						in space
Small satellite from the Technical University of Berlin to verify newly-developed satellite components.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 19, 13:41	6974	0.0013	587	605	96.60	97.61	221
2023 Feb 13, 11:44	6968	0.0012	581	598	96.47	97.40	283
Flying Laptop 2017-042G 42831						in space
Small satellite from the Institut für Raumfahrtsysteme at the University of Stuttgart, Germany built to qualify new satellite systems for space use. It carries an imaging system and a star tracker. It is also fitted with a receiver for AIS messages from ships at sea.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 19, 20:08	6974	0.0013	587	605	96.60	97.61	220
2023 Feb 13, 03:41	6968	0.0012	582	599	96.48	97.40	285
WNISat 1R (Weathernews Inc Satellite) 2017-042L 42835						in space
Small satellite monitoring Arctic sea ice and CO₂ in the atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 18, 21:34	6973	0.0012	587	604	96.59	97.61	223
Lemur-2 (Greenberg) 2017-042N 42837						in space
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and other sensors. One of four released from Cygnus OA-5 2016 Nov 25. Lemur-2 satellites are named after development and support team members. This is one of a group of eight similar satellites carried on this launch,. In order to avoid clutter the others are not listed separately. One satellite, Flock 2K-42, was not identified , indicating that it failed to activate and is among a number of unidentified items from the launch. All satellites are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 20, 17:02	6973	0.0012	586	603	96.58	97.61	216
2023 Feb 13, 01:29	6959	0.0011	574	588	96.29	97.40	272
NanoACE 2017-042V 42844						in space
3U Cubesat from Tyvak Systems acting as a technology demonstrator for satellite systems including command and control systems, guidance sytems and imaging systems.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 21, 05:52	6972	0.0012	585	602	96.55	97.61	210
2023 Feb 13, 08:32	6960	0.0010	574	589	96.31	97.40	262
Corvus BC2 2017-042X 42846						in space
6U Cubesat (3x2) - Satellite from Aquila Space in the "Landmapper" constellation of remote sensing satellites using multispecral imaging to support agriculture planning, water monitoring and land management.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 20, 18:35	6971	0.0009	587	599	96.54	97.61	213
2023 Feb 13, 01:09	6964	0.0008	581	591	96.40	97.40	271
Corvus BC1 2017-042Y 42847						in space
6U Cubesat (3x2) - Satellite from Aquila Space in the "Landmapper" constellation of remote sensing satellites using multispecral imaging to support agriculture planning, water monitoring and land management.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 21, 05:50	6971	0.0008	587	598	96.53	97.61	210
2023 Feb 13, 01:07	6964	0.0007	581	591	96.39	97.40	270
Flock 2K-1 2017-042AD 42852						Re-entered - 2022 Mar 17 Life 1707 days
3U Cubesat, part of Planet's Flock 2K cluster of imaging satellites. Flock 2K-1 is one of a swarm of 48 similar satellites carried on this launch. In order to avoid clutter the others are not listed separately. One satellite, Flock 2K-42, was not identified, indicating that it failed to activate. It is among a number of unidentified items from the launch. All Flock 2K satellites are in similar orbits.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 25, 05:49	6847	0.0011	461	476	93.97	97.00	207
CICERO 1 (Community Initiative for Cellular Earth Remote Observation) 2017-042xxx						in space
6U Cubesat (3x2), one of three launched simultaneously. Equipped to perform GPS and Galileo radio occultation observations by the Earth's atmosphere and undertake surface remote sensing by reflected navigation satellite signals. It was reported that none of the three CICERO satellites activated on separating from the launch vehicle so it was not possible to associate any of them with a catalogue number and designation.
Not Catalogued - orbit parameters unavailable
CICERO 2 (Community Initiative for Cellular Earth Remote Observation) 2017-042xxx						in space
6U Cubesat (3x2), one of three launched simultaneously. Equipped to perform GPS and Galileo radio occultation observations by the Earth's atmosphere and undertake surface remote sensing by reflected navigation satellite signals. It was reported that none of the three CICERO satellites activated on separating from the launch vehicle so it was not possible to associate any of them with a catalogue number and designation.
Not Catalogued - orbit parameters unavailable
CICERO 3 (Community Initiative for Cellular Earth Remote Observation) 2017-042xxx						in space
6U Cubesat (3x2), one of three launched simultaneously. Equipped to perform GPS and Galileo radio occultation observations by the Earth's atmosphere and undertake surface remote sensing by reflected navigation satellite signals. It was reported that none of the three CICERO satellites activated on separating from the launch vehicle so it was not possible to associate any of them with a catalogue number and designation.
Not Catalogued - orbit parameters unavailable
Ecuador-UTE-YuZGU 2017-042xxx						in space
1U CubeSat jointly developed by the Ecuadorian Universidad Tecnológica Equinoccial and the Russian Southwestern State University in Kurs as a space technology demonstrator. Low electrical power reduced its capacity to transmit so it was not possible to associate it with a catalogue number and designation.
Not Catalogued - orbit parameters unavailable
Iskra-MAI-85 2017-042xxx						in space
3U CubeSat from the Moscow Aviation Institute, created to provide students with experience in designing and manufacturing a satellite. Transmitted at low power for a while after separating from the launch vehicle but it was not possible to associate it with a catalogue number and designation.
Not Catalogued - orbit parameters unavailable
Mayak (Beacon) 2017-042xxx						in space
3U Cubesat from intended to extend four triangular reflectors, each of four square metres and intended to form a tetrahedral shape to make the satellite highly visible. The reflectors did not deploy and, as no radio transmitter was carried, it is not possible to associate it with a catalogue number and designation.
Not Catalogued - orbit parameters unavailable
MKA-N 1 2017-042xxx						in space
3U Cubesat from Russia and built by Dauria Aerospace, one of two launched simultaneously. Carried a remote sensing payload. Did not activate on separating from the launch vehicle so it is not possible to associate it with a catalogue number and designation.
Not Catalogued - orbit parameters unavailable
MKA-N 2 2017-042xxx						in space
3U Cubesat from Russia and built by Dauria Aerospace, one of two launched simultaneously. Carried a remote sensing payload. Did not activate on separating from the launch vehicle so it is not possible to associate it with a catalogue number and designation.
Not Catalogued - orbit parameters unavailable
Volga rocket stage uncatalogued						Re-entered - 2017 Jul 14 Life <1 day
Launched Canopus-Vulcan IK and other satellites. De-orbited after satellites released. Not Catalogued.
Not Catalogued - orbit parameters unavailable

2017-F04 - failed to reach orbit Simorgh (Phoenix) Ayatollah Khomeini Space Centre, Iran						2017 Jul 27, 09:30
Dummy payload?
Orbital test flight of the Simorgh rocket. Second stage failed.

2017-043 Soyuz-FG 11A511U-FG Baikonur Cosmodrome						2017 Jul 28, 15:41
Soyuz MS-05 (Soyuz 11F732A48 № 736) 2017-043A 42898						Re-entered - 2017 Dec 14 Life 139 days Returned to Earth
Carrying crew to ISS - Sergei Ryazansky (Roscosmos, Randolph Bresnik (NASA) and Paolo Nespoli (ESA). Docked with the Rassvet module of the ISS Jul 28 at 21:54 UTC, seven minutes earlier than planned. Undocked, carrying its original crew, 2017 Dec 14 at 05:14 UTC. Retro-fire at 07:44 UTC was followd by landing in Kazakhstan, 147 kilometers south east of Dzhezkazgan, at 08:37 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 29, 13:24	6783	0.0006	400	409	92.65	51.64	86
Soyuz upper stage 2017-043B 42899						Re-entered - 2017 Aug 1 Life 4 days
Launched Soyuz MS-05.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Jul 28, 21:23	6582	0.0018	192	215	88.57	51.64	107

2017-044 Vega (VV-10) Centre Spatiale Guyanaise						2017 Aug 2, 01:58
OptSat 3000 2017-044A 42900						in space
High resolution Earth observation satellite owned by the Italian Ministry of Defense. Separated from the launch vehicle at 02:43:22 UTC. Orbit information is based on amateur observation with the exception of 2023 August when Space-Track inadvertently released data by mis-identifying it as an object from the 2023 Aug 3 launch of Fengyun 3F (2023-111C) into the same orbit plane.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Aug 6, 21:32	6829	0.0002	450	453	93.61	97.20	330	10:30
2018 May 5, 21:42	6824	0.0010	439	453	93.50	97.22	332	10:27
2018 May 7, 20:37	6837	0.0013	450	468	93.77	97.22	35	10:27
2019 May 12, 21:15	6833	0.0031	434	476	93.69	97.22	270	10:21
2019 May 13, 20:52	6866	0.0022	473	503	94.37	97.31	36	10:21
2023 Apr 17, 22:40	6849	0.0006	467	475	94.01	97.34	170	09:45
2023 Aug 3, 08:25	6869	0.0015	480	501	94.42	97.37	218	09:45
Venus 2017-044B 42901						in space
Joint mission by the Israel Space Agency and CNES, studying evolution of vegetation on the Earth's surface and monitoring the environment. It has a technological element to provide in-flight qualification for an Israeli Electrical Propulsion System. Separated from the launch vehicle at 02:35:50 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Aug 4, 18:28	7100	0.0003	720	724	99.24	98.35	138	10:30
2017 Aug 9, 20:56	7101	0.0004	720	726	99.26	98.35	143	10:30
2017 Aug 12, 03:34	7102	0.0001	723	724	99.27	98.35	132	10:30
2023 Feb 13, 14:00	6942	0.0021	550	578	95.94	97.52	176	10:19
Vega upper stage (AVUM) 2017-044C 42902						Re-entered - 2020 Sep 11 Life 1136 days
Launched OPTUS 3000 and Venus.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 3, 10:44	6823	0.0008	440	451	93.48	97.22	342

2017-045 Falcon 9 v1.2 Kennedy Space Center						2017 Aug 14, 16:31
SpaceX Dragon CRS-12 2017-045A 42904						Re-entered - 2017 Sep 17 Life 34 days Returned to Earth
Carrying a cargo to the ISS under NASA's Commercial Resupply Services (CRS) contract. Captured by the ISS Remote Manipulator System Aug 16 at 10:52 UTC and attached to the lower port of the Harmony module at 13:17 UTC. Undocked using the RMS and released Jul 3 at 080:40 UTC. Retro-fire led to splashdown at 14:14 UTC in the Pacific Ocean, about 300 km SW of Baja, California.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 14, 16:54	6658	0.0117	203	358	90.12	51.63	47
2017 Aug 16, 09:55	6783	0.0006	401	408	92.65	51.64	144
Falcon 9 upper stage uncatalogued						Re-entered - 2017 Aug 14 Life <1 day
Launched SpaceX Dragon CRS-12. De-orbited soon after spacecraft separation. Not catalogued.
Not Catalogued - orbit parameters unavailable

2017-046 Proton-M + Briz-M Baikonur Cosmodrome						2017 Aug 16, 22:07
Cosmos 2520 (Blagovest, 14F149 № 11L) 2017-046A 42907						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Aug 17, 02:09	24459	0.7227	404	35758	634.47	48.68	360
2017 Aug 18, 21:53	42014	0.0030	35512	35760	1428.41	0.08	193	57°.5 E
2017 Aug 29, 14:09	42165	0.0003	35775	35798	1436.09	0.02	49	76°.5 E
2017 Aug 30, 06:54	42254	0.0030	35749	36003	1440.64	0.11	202
2017 Sep 11, 19:02	42221	0.0012	35792	35893	1438.95	0.03	204	46°.8 E
2017 Sep 19, 00:20	42163	0.0002	35778	35793	1436.02	0.03	224	45°.1 E
2023 Feb 11, 23:26	42164	0.0001	35783	35789	1436.06	0.04	225	45°.0 E
Briz-M rocket stage 2017-046C 42909						in space
Launched Cosmos 2520.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 18, 00:00	45205	0.0679	35759	41895	1594.19	0.11	140
Briz-M APT 2017-046B 42908						in space
Propellant tank discarded by Briz-M.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 19, 06:31	24428	0.7225	400	35700	633.28	48.66	0

2017-I26 Manual release during EVA International Space Station						2017 Aug 17, 15:10
Tomsk-TPU 120 1998-067MZ 42910						Re-entered - 2019 Oct 20 Life 794 days
3U Cubesat from developed by students at the Tomsk Polytechnic University, Russia. The satellite was printed in 3D as a technology demonstrator. One of a group of five satellites released over a twenty minute period during a Russian EVA.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 18, 14:24	6781	0.0008	397	408	92.61	51.64	158
YuZGU № 1 (Tanyusha 1) 1998-067NA 42911						Re-entered - 2019 Jul 30 Life 712 days
3U Cubesat from Russia's Southwest State University at Kursk and built by students, carrying an amateur radio payload. One of a group of five satellites released over a twenty minute period during a Russian EVA.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 18, 14:24	6781	0.0008	397	408	92.61	51.64	154
YuZGU № 2 (Tanyusha 2) 1998-067NB 42912						Re-entered - 2019 Sep 8 Life 752 days
3U Cubesat from Russia's Southwest State University at Kursk and built by students, carrying an amateur radio payload. One of a group of five satellites released over a twenty minute period during a Russian EVA.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 18, 14:24	6781	0.0007	398	408	92.62	51.64	165
Sfera 2 (Vektor-T) 1998-067NC 42913						Re-entered - 2018 Nov 29 Life 469 days
Small, inert spherical satellite used to study atmospheric drag. One of a group of five satellites released over a twenty minute period during a Russian EVA.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 18, 14:46	6781	0.0007	398	407	92.62	51.64	172
TNS-0 2 1998-067ND 42914						Re-entered - 2019 Oct 15 Life 789 days
Technology satellite from Russia. Purpose unknown. One of a group of five satellites released over a twenty minute period during a Russian EVA.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 18, 20:34	6781	0.0007	399	408	92.62	51.64	153

2017-047 Atlas V 401 Cape Canaveral Air Force Station						2017 Aug 18, 12:29
TDRS 13 (Tracking and Data Relay Satellite) 2017-047A 42915						in space
Final launch of third generation comsat, part of the space-based portion of NASA's Space Network, relaying signals from satellites and spacraft in low Earth orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Aug 18, 15:57	26578	0.5852	4647	35753	718.70	26.21	180
2017 Aug 21, 12:55	29542	0.4265	10563	35765	842.21	17.55	181
2017 Aug 23, 06:22	35281	0.1954	22008	35798	1099.18	10.59	179
2017 Aug 25, 10:33	40351	0.0448	32164	35782	1344.43	7.75	180
2017 Aug 27, 13:22	41917	0.0059	35291	35786	1423.46	7.11	180
2017 Aug 28, 14:05	42138	0.0008	35727	35792	1434.71	7.08	222	149°.7 W
2017 Aug 30, 03:44	42167	0.0003	35777	35802	1436.23	7.00	334	149°.7 W
2023 Feb 13, 04:26	42165	0.0015	35725	35848	1436.10	4.15	106	11°.7 W
Atlas V upper stage (Centaur) 2017-047B 42916						in space
Launched TDRS 13.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 18, 18:41	26037	0.5824	4494	34824	696.87	26.42	179

2017-048 H-IIA 204 (F-35) Tanegashima Space Centre						2017 Aug 19, 05:29
Michibiki 3 (QZSS 3) 2017-048A 42917						in space
Quasi Zenith Satellite System satellite providing a timing and positioning service to improve navigational accuracy for users in Japan from a combination of equatorial GEO and inclined GEO, giving coverage to areas where the topography works against GPS reception. “Michibiki" translates into English as "Showing the Way".
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Aug 19, 17:03	24207	0.7235	315	35344	624.71	19.94	179
2017 Aug 22, 18:55	35319	0.1964	22005	35878	1100.97	2.33	179
2017 Aug 23, 12:21	40193	0.0509	31767	35862	1336.53	0.43	181
2017 Aug 24, 16:21	42146	0.0018	35690	35845	1435.14	0.10	14	126°.4 E
2017 Aug 28, 15:25	42164	0.0005	35764	35808	1436.06	0.09	32	127°.0 E
2023 Feb 12, 15:07	42167	0.0002	35780	35797	1436.19	0.06	152	126°.9 E
H-IIA upper stage 2017-048B 42918						in space
Launched Michibiki 3.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 19, 11:20	24506	0.7248	365	35891	636.30	19.95	179

2017-049 Falcon 9 v1.2 Vandenberg Air Force Base						2017 Aug 24, 18:51
Formosat 5 (Cosmic 5) 2017-049A 42920						in space
Earth imaging satellite from the National Space Organization (NSPO) of Taiwan. Also carries the Advanced Ionospheric Probe (AIP), for studies of ionospheric plasma physics.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Aug 25, 02:34	7101	0.0009	717	730	99.26	98.29	231
2023 Feb 13, 02:56	7101	0.0010	716	730	99.25	98.33	227
Falcon 9 upper stage uncatalogued						Re-entered - 2017 Aug 24 Life <1 day
Launched Formosat 5. De-orbited soon after satellite separation. Not catalogued.
Not Catalogued - orbit parameters unavailable

2017-050 Minotaur IV Cape Canaveral Air Force Station						2017 Aug 26, 06:04
Sensorsat (ORS-5) 2017-050A 42921						in space
Satellite from the USAF Space Rapid Capabilities Office (formerly known as Operationally Responsive Space - ORS). Carries sensors to detect and monitor satellites in the geosynchronous belt.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2018 Jun 6, 21:32	6974	0.0006	592	601	96.61	0.08	358
Minotaur stage 2017-050E 42925						in space
Launched Sensorsat (ORS-5).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 27, 22:22	6975	0.0010	590	603	96.62	0.05	171
Minotaur upper stage 2017-050G 42927						Re-entered - 2024 Feb 12 Life 2361 days
Launched Sensorsat (ORS-5).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 31, 16:07	6871	0.0159	384	603	94.47	24.53	62

2017-051 PSLV-XL (PSLV C-39) Satish Dhawan Space Centre						2017 Aug 31, 13:30
IRNSS 1H + PSLV upper stage 2017-051A 42928						Re-entered - 2019 Mar 2 Life 548 days
Intended to be the eigth satellite in India's Regional Navigation System. I was to replace IRNSS 1A (2013-034A/39199) and to complete the constellation. It was lost when a mechanical problem left it attached to the launch vehicle upper stage.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Aug 31, 20:31	9741	0.3286	162	6563	159.47	19.15	167

2017-052 Falcon 9 v1.2 Kennedy Space Center						2017 Sep 7, 14:00
USA 277 (OTV-5, X-37B#2 Flight 3) 2017-052A 42932						Re-entered - 2019 Oct 27 Life 780 days Returned to Earth
Flight of USAF/Boeing X-37B space plane. The vehicle is described as a space technology demonstrator and host platform for experimental payloads. This mission also carried a number of small satellite ride share payloads but there is no indication of how or when they were released into independent orbit. Launch was by SpaceX on behalf of the USAF Rapid Capabilities Office. Landed Kennedy Space Center Shuttle Landing Facility 2019 Oct 27 at 07:51 UTC.. Element sets were not released by Space-Track so parameters are based on amateur observation, the final one was calculated by Nico Janssen from radio observations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2018 Apr 13, 01:59	6734	0.0003	353	358	91.65	54.48	306
2018 Apr 21, 21:40	6695	0.0010	310	323	90.86	54.51	167
2018 Aug 19, 19:06	6703	0.0005	322	329	91.04	54.51	235
2018 Aug 25, 20:24	6769	0.0035	368	415	92.38	54.50	166
2018 Nov 3, 17:03	6722	0.0009	338	350	91.42	54.53	169
2019 Feb 26, 00:39	6696	0.0003	316	319	90.88	54.51	246
2019 Oct 8, 04:57	6695	0.0010	310	324	90.87	54.51	219
2019 Oct 27, 01:37	6652	0.0001	274	275	90.00	54.52	285
USA 295 2017-052C 45169						Re-entered - unknown date
Satellite of unknown purpose. Neither formally acknowledged nor catalogued until 2020 February 11. A US filing for the satellite lodged with the United Nations in 2020 and published early 2021 listed the inclination as 56°.9 and the orbit height as 182 x 356 km. The inclination suggests release from the Falcon 9 into a similar orbit (around 350 km) as USA 277 (OTV-5).
Orbit classified as 'Secret' - data withheld
USA 296 2017-052D 45170						Re-entered - unknown date
Satellite of unknown purpose. Neither formally acknowledged nor catalogued until 2020 February 11. A US filing for the satellite lodged with the United Nations in 2020 and published early 2021 listed the inclination as 56°.9 and the orbit height as 182 x 356 km. The inclination suggests release from the Falcon 9 into a similar orbit (around 350 km) as USA 277 (OTV-5).
Orbit classified as 'Secret' - data withheld
USA 297 2017-052E 45171						Re-entered - unknown date
Satellite of unknown purpose. Neither formally acknowledged nor catalogued until 2020 February 11. A US filing for the satellite lodged with the United Nations in 2020 and published early 2021 listed the inclination as 56°.9 and the orbit height as 182 x 356 km. The inclination suggests release from the Falcon 9 into a similar orbit (around 350 km) as USA 277 (OTV-5).
Orbit classified as 'Secret' - data withheld
Falcon 9 upper stage 2017-052B 42933						Re-entered - 2017 Sep 7 Life <1 day
Launched USA 277 (OTV-5/X-37B). Manoeuvred to 63° inclination orbit after releasing OTV-5, possibly as a re-start/burn test. Released the three smaller USA satellites carried on the launch. Caused to re-enter above the Indian Ocean about four hours after launch on its third circuit of the Earth.
Orbit classified as 'Secret' - data withheld

2017-053 Proton-M + Briz-M Baikonur Cosmodrome						2017 Sep 11, 19:23
Amazonas 5 2017-053A 42934						in space
Communications satellite serving satellite television platforms in Latin America and Brazil. Expected location - 61° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Sep 13, 11:21	26194	0.5900	4361	35272	703.19	22.85	0
2017 Sep 15, 03:03	29101	0.4313	10172	35275	823.44	12.38	1
2017 Sep 15, 18:23	36337	0.1979	22767	37152	1148.92	3.88	11
2017 Sep 18, 14:00	42174	0.0004	35779	35812	1436.55	0.23	310	71°.8 W
2017 Sep 19, 03:48	41874	0.0056	35262	35731	1421.28	0.08	190
2017 Sep 22, 01:00	42089	0.0018	35634	35788	1432.23	0.07	139	59°.0 W
2017 Sep 25, 03:01	42164	0.0001	35784	35788	1436.08	0.08	354	58°.3 W
2018 May 8, 12:58	42165	0.0004	35770	35803	1436.10	0.03	64	61°.0 W
2023 Feb 12, 12:42	42165	0.0005	35765	35809	1436.12	0.04	23	61°.0 W
Briz-M rocket stage 2017-053B 42935						in space
Launched Amazonas 5.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Sep 13, 07:59	25035	0.5945	3773	33542	657.04	23.26	3
Briz-M APT 2017-053C 42936						in space
Propellant tank discarded by Briz-M.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Sep 12, 03:36	14007	0.5216	323	14936	274.98	49.53	353

2017-054 Soyuz-FG 11A511U-FG Baikonur Cosmodrome						2017 Sep 12, 21:17
Soyuz MS-06 (Soyuz 11F732A48 № 734) 2017-054A 42937						Re-entered - 2018 Feb 28 Life 169 days Returned to Earth
Carrying crew to ISS - Aleksandr Misurkin (Roscosmos) plus Mark Vande and Joe Acaba of NASA. Docked with the Poisk module of the ISS Sep 13 at 02:55 UTC, two minutes earlier than planned. Undocked, carrying its original crew, 2018 Feb 27 at 23:08 UTC. Retro-fire at 4:39 UTC was followd by landing in Kazakhstan, 146 kilometers south east of Dzhezkazgan, at 02:31:21 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Sep 12, 23:18	6598	0.0048	188	252	88.90	51.64	96
2017 Sep 13, 01:55	6763	0.0026	367	402	92.24	51.64	12
2017 Sep 14, 13:23	6783	0.0004	402	407	92.65	51.64	272
Soyuz upper stage 2017-054B 42938						Re-entered - 2017 Sep 15 Life 3 days
Launched Soyuz MS-06.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Sep 12, 21:45	6595	0.0037	192	241	88.83	51.66	99

2017-055 Soyuz-2.1b + Fregat Plesetsk Cosmodrome						2017 Sep 22, 00:02
Cosmos 2522 (Uragan-M № 752) 2017-055A 42939						in space
GLONASS-M navigation satellite to fill a space in the constellation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Sep 23, 05:27	25519	0.0007	19124	19158	676.18	64.81	270
2017 Sep 28, 09:14	25559	0.0011	19154	19208	677.76	64.81	39
2017 Oct 5, 18:46	25516	0.0007	19119	19157	676.06	64.81	264
2017 Oct 13, 07:17	25508	0.0010	19104	19156	675.73	64.80	250
Fregat rocket stage 2017-055B 42940						in space
Launched Cosmos 2522.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 17, 03:07	25952	0.0122	19257	19892	693.47	64.76	129

2017-056 Atlas V 541 Vandenberg Air Force Base						2017 Sep 24, 05:49
USA 278 2017-056A 42941						in space
USA Government/Military satellite, possibly for electronic intelligence gathering (ELINT). Orbits based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 6, 02:05	26294	0.6741	2190	37642	707.22	63.70	269
2017 Oct 12, 00:01	26556	0.6767	2206	38149	717.79	63.66	269
Atlas V upper stage (Centaur) uncatalogued						Re-entered - 2017 Sep 24 Life <1 day
Launched USA-278. Caused to re-enter above southern Indian Ocean soon after releasing the satellite.
Not Catalogued - orbit parameters unavailable

2017-057 Proton-M + Briz-M Baikonur Cosmodrome						2017 Sep 28, 18:52
Asiasat 9 2017-057A 42942						in space
Comsat providing direct to home TV, video distribution, private networks and broadband services across the Asia-Pacific region. Expected location 122° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Sep 29, 23:45	26279	0.6047	4010	35790	706.58	23.36	0
2017 Oct 1, 15:09	29110	0.4487	9672	35793	823.82	12.64	0
2017 Oct 2, 14:02	33286	0.2667	18030	35786	1007.29	4.79	1
2017 Oct 5, 18:08	42101	0.0012	35672	35773	1432.82	0.07	23	118°.8 E
2017 Oct 10, 22:04	42164	0.0002	35778	35793	1436.06	0.05	222	121°.6 E
2023 Feb 13, 00:53	42165	0.0002	35778	35796	1436.11	0.00	158	122°.1 E
Briz-M rocket stage 2017-057B 42943						in space
Launched Asiast 9.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 2, 04:42	25365	0.6085	3552	34421	670.05	23.79	3

2017-058 CZ 2C Xichang Space Centre						2017 Sep 29, 04:21
Yaogan 30-01A 2017-058A 42945						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Sep 29, 12:12	6975	0.0007	592	601	96.62	35.01	204
2017 Oct 23, 04:44	6978	0.0004	597	603	96.68	35.00	275
2023 Feb 13, 10:26	6972	0.0004	590	596	96.55	35.00	356
2025 Feb 24, 09:57	6949	0.0004	568	573	96.07	35.00	283
Yaogan 30-01B 2017-058B 42946						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Sep 29, 12:11	6975	0.0006	593	601	96.62	35.00	226
2017 Oct 24, 21:29	6978	0.0002	599	601	96.68	35.00	112
2023 Feb 13, 09:22	6972	0.0002	592	595	96.55	35.00	202
2025 Feb 24, 10:24	6948	0.0001	570	571	96.07	35.00	149
Yaogan 30-01C 2017-058C 42947						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Sep 29, 11:54	6975	0.0006	593	601	96.63	35.00	208
2017 Oct 8, 06:37	6986	0.0005	605	612	96.86	34.99	141
2017 Oct 29, 01:46	6978	0.0006	595	604	96.68	35.00	7
2023 Feb 13, 11:23	6971	0.0006	589	598	96.55	35.00	36
2025 Feb 24, 10:09	6945	0.0006	563	571	96.00	35.00	329
CZ 2C second stage 2017-058D 42948						in space
Launched cluster of three Yaogan-30 satellites. Orbit adjusted after satellite release.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Sep 29, 12:16	7009	0.0068	583	678	97.33	34.93	255

2017-059 Ariane 5ECA (VA-239) Centre Spatiale Guyanaise						2017 Sep 29, 21:56
Intelsat 37e 2017-059A 42950						in space
Communications satellite for fixed and mobile services across the Americas, Africa and Europe. Expected location - 18° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Oct 2, 13:16	24319	0.7269	264	35618	629.06	5.93	180
2017 Oct 4, 16:57	25423	0.6562	2362	35728	672.34	3.76	180
2017 Oct 6, 06:18	25868	0.6282	3239	35740	690.07	3.18	180
2017 Oct 14, 11:46	36280	0.1618	24030	35773	1146.18	0.13	157
2017 Oct 20, 19:06	41721	0.0102	34916	35770	1413.50	0.04	75
2017 Oct 24, 18:09	42146	0.0004	35753	35783	1435.15	0.03	192	84°.7 E
2017 Oct 26, 12:09	42167	0.0002	35781	35796	1436.19	0.02	255	84°.5 E
2018 Feb 1, 10:04	42575	0.0003	36185	36210	1457.13	0.06	99
2018 Feb 26, 18:00	42163	0.0003	35772	35797	1435.98	0.12	222	18°.2 W
2023 Feb 12, 09:28	42165	0.0003	35776	35797	1436.10	0.02	216	18°.0 W
BSat-4a 2017-059B 42951						in space
Japanese broadcast comsat providing high definition television services. Expected location - 110°east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Oct 1, 00:39	24357	0.7273	263	35693	630.50	5.96	179
2017 Oct 2, 17:51	32949	0.2778	17416	35725	992.00	1.13	177
2017 Oct 4, 13:42	41174	0.0231	33845	35746	1385.76	0.03	136
2017 Oct 5, 09:01	42111	0.0003	35721	35746	1433.37	0.06	44	101°.9 E
2017 Oct 9, 12:31	42165	0.0011	35739	35836	1436.12	0.04	181	103°.9 E
2017 Oct 30, 03:19	42100	0.0001	35719	35725	1432.80	0.02	34	105°.5 E
2017 Nov 5, 23:28	42146	0.0016	35701	35834	1435.12	0.02	179	110°.8 E
2017 Nov 8, 13:22	42164	0.0001	35783	35788	1436.06	0.01	103	109°.8 E
2023 Feb 9, 08:04	42165	0.0004	35770	35803	1436.10	0.04	337	109°.8 E
Ariane 5 upper stage (VA-239) 2017-059C 42952						in space
Launched Intelsat 37E and BSat 4A.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Sep 29, 16:53	24396	0.7275	270	35765	632.03	5.98	178

2017-060 CZ 2D Jiuquan Space Centre						2017 Oct 9, 04:13
VRSS 2 (Venezuelan Remote Sensing Satellite 2) 2017-060A 42954						in space
Remote sensing satellite to study Venezuelan territory in support of planning, agriculture and disaster recovery.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Oct 9, 10:26	7020	0.0018	629	655	97.56	98.03	288	10:30
2017 Oct 9, 19:56	7020	0.0018	630	655	97.56	98.02	285	10:30
2023 Feb 13, 11:38	7017	0.0020	625	653	97.50	97.82	108	09:55
CZ 2D second stage uncatalogued						Re-entered - 2017 Oct 9 Life <1 day
Launched VRSS 2. De-orbited soon after satellite release. Not catalogued.
Not Catalogued - orbit parameters unavailable

2017-061 Falcon 9 v1.2 Vandenberg Air Force Base						2017 Oct 9, 12:37
Iridium 133 (Iridium Next) 2017-061A 42955						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 9, 18:55	6998	0.0010	612	627	97.09	86.68	225
2017 Oct 14, 11:00	7087	0.0000	708	708	98.95	86.52	213
2017 Oct 25, 10:11	7156	0.0001	777	779	100.40	86.40	78
Iridium 100 (Iridium Next) 2017-061B 42956						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 9, 18:29	6997	0.0010	612	626	97.09	86.69	224
2017 Oct 31, 10:02	7156	0.0002	776	779	100.40	86.40	87
Iridium 122 (Iridium Next) 2017-061C 42957						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 9, 18:52	6997	0.0010	612	626	97.09	86.69	221
2017 Oct 27, 08:09	7156	0.0001	777	778	100.40	86.40	87
Iridium 129 (Iridium Next) 2017-061D 42958						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 10, 07:50	6997	0.0014	609	629	97.08	86.70	218
2017 Nov 2, 10:27	7156	0.0003	776	779	100.40	86.40	87
Iridium 119 (Iridium Next) 2017-061E 42959						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 10, 00:58	6997	0.0011	611	626	97.08	86.68	219
2017 Oct 25, 22:39	7081	0.0002	702	704	98.83	86.52	59
2017 Nov 6, 22:31	7156	0.0001	777	779	100.40	86.40	91
Iridium 107 (Iridium Next) 2017-061F 42960						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 10, 08:00	6996	0.0011	610	626	97.07	86.68	218
2017 Nov 2, 11:26	7081	0.0003	701	705	98.84	86.53	108
2017 Nov 8, 11:49	7156	0.0002	776	779	100.40	86.40	89
Iridium 132 (Iridium Next) 2017-061G 42961						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 10, 00:57	6997	0.0011	610	626	97.07	86.68	219
2017 Oct 21, 08:04	7082	0.0001	703	705	98.86	86.52	85
2017 Nov 4, 04:09	7156	0.0002	776	779	100.40	86.40	100
Iridium 136 (Iridium Next) 2017-061H 42962						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 9, 20:06	6996	0.0012	610	627	97.06	86.68	214
2017 Oct 25, 09:45	7081	0.0001	702	704	98.84	86.52	73
2017 Nov 12, 20:33	7156	0.0002	776	779	100.40	86.40	95
Iridium 139 (Iridium Next) 2017-061J 42963						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 10, 02:35	6996	0.0012	610	626	97.06	86.68	218
2017 Oct 26, 11:35	7081	0.0002	701	705	98.84	86.52	76
2017 Nov 10, 21:49	7156	0.0002	776	779	100.40	86.40	97
Iridium 125 (Iridium Next) 2017-061K 42964						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 10, 07:50	6996	0.0012	610	626	97.06	86.68	216
2017 Oct 29, 21:32	7081	0.0002	701	704	98.83	86.53	62
2017 Nov 16, 04:46	7156	0.0002	776	779	100.40	86.40	89
Falcon 9 upper stage uncatalogued						Re-entered - 2017 Oct 9 Life <1 day
Launched cluster of Iridium satellites.
Not Catalogued - orbit parameters unavailable

2017-062 H-IIA 202 (F-36) Tanegashima Space Centre						2017 Oct 9, 22:01
Michibiki 4 (QZSS 4) 2017-062A 42965						in space
Quasi Zenith Satellite System satellite providing a timing and positioning service to improve navigational accuracy for users in Japan from a combination of equatorial GEO and inclined GEO, giving coverage to areas where the topography works against GPS reception. “Michibiki" translates into English as "Showing the Way".
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Oct 11, 03:17	27970	0.5143	7208	35977	775.91	36.46	181
2017 Oct 12, 14:06	40208	0.0534	31684	35975	1337.27	40.22	178
2017 Oct 14, 12:00	42314	0.0019	35855	36017	1443.72	40.44	107
2017 Oct 18, 05:49	42164	0.0747	32637	38935	1436.07	40.47	270	134°.0 E
H-IIA upper stage 2017-062B 42966						in space
Launched Michibiki 4.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 11, 21:09	24191	0.7241	297	35330	624.09	31.84	181

2017-063 Falcon 9 v1.2 Kennedy Space Center						2017 Oct 11, 22:53
Echostar 105/SES 11 2017-063A 42967						in space
Dual payload comsat with sets of transponders from Echostar and SES serving the continental USA, the Gulf of Mexico and the the Caribbean. Expected location 105° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Oct 13, 05:50	26781	0.7505	304	40500	726.92	27.81	179
2017 Oct 13, 18:46	29269	0.6007	5310	40471	830.55	15.54	178
2017 Oct 15, 08:24	37756	0.2411	22274	40481	1216.84	3.56	178
2017 Oct 16, 15:20	44451	0.0543	35657	40489	1554.48	0.58	172
2017 Oct 18, 05:15	42165	0.0033	35648	35926	1436.12	0.07	123	141°.8 W
2017 Nov 5, 18:22	42113	0.0013	35678	35791	1433.43	0.07	296	142°.2 W
2017 Nov 6, 16:21	41973	0.0000	35594	35595	1426.30	0.06	253
2017 Nov 22, 12:43	42164	0.0001	35782	35790	1436.08	0.04	269	104°.9 W
2023 Feb 13, 09:09	42165	0.0003	35776	35797	1436.11	0.06	32	104°.9 W
Falcon 9 upper stage 2017-063B 42968						in space
Launched Echostar 105.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 13, 17:55	26796	0.7504	311	40525	727.55	27.87	179

2017-064 Rockot Plesetsk Cosmodrome						2017 Oct 13, 09:27
Sentinel 5P (Sentinel 5 Precursor) 2017-064A 42969						in space
Atmospheric monitoring satellite to fill in the data gap and provide data continuity between the retirement of the Envisat satellite and NASA's Aura mission, and the launch of Sentinel-5
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Oct 13, 15:53	7196	0.0002	816	819	101.25	98.72	78	01:30
2017 Nov 11, 19:31	7205	0.0004	824	830	101.44	98.71	53	01:30
Briz-KM rocket stage 2017-064B 42970						in space
Launched Sentinel 5P.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 13, 20:29	6968	0.0253	413	767	96.48	98.74	307

2017-065 Soyuz-2.1a Baikonur Cosmodrome						2017 Oct 14, 08:46
Progress MS-07 (Progress 7K-MS №437) 2017-065A 42971						Re-entered - 2018 Apr 26 Life 194 days
Supplies to ISS. Docked with the downward-facing port of Pirs 2017 Oct 16 at 11:04 UTC. Undocked 2018 Mar 28 at13:50:30 UTC. Progress MS-07 then spent four weeks in independent orbit conducting studies of the Earth's atmosphere, and microgravity conditions aboard the spacecraft. Retro-fire Apr 26 at 04:08 UTC led to destructive re-entry at 04:42 UTC. Any remaining fragments impacted the southern Pacific Ocean around 04:51 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 14, 09:17	6581	0.0026	185	220	88.54	51.62	67
2017 Oct 14, 14:57	6698	0.0024	304	336	90.92	51.64	217
2017 Oct 15, 08:41	6697	0.0016	308	329	90.90	51.64	214
Soyuz upper stage 2017-065B 42972						Re-entered - 2017 Oct 16 Life 2 days
Launched Progress MS-07.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 14, 14:29	6579	0.0024	185	217	88.51	51.65	69

2017-066 Atlas V 421 Cape Canaveral Air Force Station						2017 Oct 15, 07:28
USA 279 (SDS-4 F1?) 2017-066A 42949						in space
Possible first in the fourth generation of the Satellite Data System (SDS) relaying signals from military satellites in low Earth orbit. The NORAD catalogue number for this mission is out of sequence and was probably allocated an unused 'slot' reserved for a satellite or debris item that subsequently did not appear. Orbits are based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 19, 09:01	27396	0.5388	6257	35780	752.14	12.72	180
2017 Oct 21, 22:02	38614	0.0945	28587	35886	1258.59	5.88	181
2017 Dec 18, 09:39	42165	0.0002	35779	35795	1436.12	4.89	301
Atlas V upper stage (Centaur) uncatalogued						Re-entered - 2017 Oct 15 Life <1 day
Launched USA 279. Retro-fire Oct 15 around 08:30 UTC caused it to re-enter above the central Pacific Ocean at around 16:00 UTC before completing a circuit of the Earth. Not catalogued. Orbit is based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 15, 11:28	20274	0.6975	-245	28037	478.81	18.89	167

2017-I27 NanoRacks Kaber Microsat Deployer International Space Station						2017 Oct 24, 09:45
Kestrel Eye (Kestrel Eye IIM) 1998-067NE 42982						Re-entered - 2021 Aug 28 Life 1404 days
Small satellite carrying an optical imaging system system including a commercial off-the-shelf (COTS) telescope. Built to demonstrate the capabilities of a small satellte.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 24, 21:17	6782	0.0006	400	408	92.64	51.64	52

2017-I28 NanoRacks Kaber Microsat Deployer International Space Station						2017 Oct 27, 09:15
SIMPL (Satlet Initial-Mission Proofs and Lessons) 1998-067NF 42983						Re-entered - 2022 Jul 26 Life 1733 days
Satellite to demonstrate that larger vehicles can be assembled from small “Satlets”. SIMPL consists of six Satlets that were joined together aboard ISS before release into orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Oct 28, 09:54	6782	0.0006	400	408	92.64	51.64	52

2017-067 Falcon 9 v1.2 Kennedy Space Center						2017 Oct 30, 19:34
ANASIS-I (Koreasat 5A) 2017-067A 42984						in space
South Korean communications satellite. Expected location 113° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Oct 30, 21:17	31613	0.7892	285	50185	932.32	22.04	179
2017 Nov 9, 17:26	42264	0.0012	35836	35935	1441.15	0.03	44
2017 Nov 13, 08:32	42194	0.0008	35784	35849	1437.61	0.18	225	114°.6 E
2017 Nov 14, 14:01	42164	0.0000	35784	35787	1436.05	0.04	26	114°.6 E
2018 Feb 9, 07:10	42166	0.0001	35785	35791	1436.16	0.01	220	113°.1 E
2023 Feb 13, 14:08	42165	0.0001	35782	35791	1436.09	0.03	247	113°.2 E
Falcon 9 upper stage 2017-067B 42985						Re-entered - 2018 Oct 27 Life 362 days
Launched Koreasat 5A.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 9, 03:53	31540	0.7886	289	50035	929.10	22.06	183

2017-068 Minotaur-C 3210 Vandenberg Air Force Base						2017 Oct 31, 21:37
Skysat 13 (Skysat C11) 2017-068A 42987						in space
Commercial imaging satellite from Planet Labs providing high resolution images and video.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 1, 00:31	6891	0.0023	497	529	94.88	97.35	212
2017 Nov 6, 10:00	6893	0.0020	500	529	94.91	97.35	196
2023 Feb 13, 14:01	6828	0.0002	448	451	93.57	97.31	191
Skysat 12 (Skysat C10) 2017-068B 42988						in space
Commercial imaging satellite from Planet Labs providing high resolution images and video.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 1, 00:31	6890	0.0023	496	528	94.87	97.36	214	13:14
2017 Nov 6, 08:24	6892	0.0020	500	528	94.91	97.35	197	13:14
Skysat 11 (Skysat C9) 2017-068C 42989						in space
Commercial imaging satellite from Planet Labs providing high resolution images and video.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 1, 00:31	6891	0.0022	497	528	94.87	97.36	214	13:14
2017 Nov 6, 09:59	6892	0.0020	500	528	94.91	97.35	197	13:14
2023 Feb 13, 14:16	6828	0.0001	449	450	93.57	97.31	59	13:33
Skysat 10 (Skysat C8) 2017-068D 42990						in space
Commercial imaging satellite from Planet Labs providing high resolution images and video.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 1, 00:31	6891	0.0022	498	527	94.88	97.36	215	13:14
2017 Nov 6, 13:09	6892	0.0020	500	528	94.90	97.35	197	13:14
2023 Feb 13, 03:43	6828	0.0001	449	450	93.57	97.31	94	13:39
Skysat 9 (Skysat C7) 2017-068E 42991						in space
Commercial imaging satellite from Planet Labs providing high resolution images and video.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 1, 00:31	6891	0.0021	499	527	94.88	97.36	215	13:14
2017 Nov 6, 13:08	6892	0.0020	500	527	94.90	97.35	198	13:14
2023 Feb 13, 02:55	6828	0.0003	447	451	93.57	97.31	191	13:40
Skysat 8 (Skysat C6) 2017-068F 42992						in space
Commercial imaging satellite from Planet Labs providing high resolution images and video.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 1, 00:31	6891	0.0020	499	527	94.88	97.36	217	13:14
2017 Nov 6, 13:08	6892	0.0019	500	527	94.90	97.35	199	13:14
Flock 3M-1 2017-068J 42995						Re-entered - 2023 Mar 24 Life 1970 days
3U Cubesat, part of Planet's Flock 3M cluster of imaging satellites. The satellite is one of a cluster of four Flock 3M 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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 7, 09:39	6890	0.0017	500	524	94.86	97.34	198
2023 Feb 13, 01:59	6756	0.0012	369	385	92.10	97.43	277
Minotaur-C upper stage 2017-068H 42994						Re-entered - 2025 Jan 4 Life 2622 days
Launched Skysat C6 - C11 group and other satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 1, 19:42	6891	0.0018	500	525	94.88	97.35	217

2017-069 CZ 3B + YZ-1 Xichang Space Centre						2017 Nov 5, 11:45
Beidou 24 (Beidou-3 M-1) 2017-069A 43001						in space
Phase 2 operational satellite in MEO for China's navigation satellite system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 6, 21:50	28156	0.0086	21535	22020	783.62	55.00	178
2017 Nov 12, 17:05	27906	0.0008	21506	21549	773.23	55.01	281
2023 Feb 12, 15:23	27906	0.0011	21498	21558	773.23	55.70	288
Beidou 25 (Beidou-3 M-2) 2017-069B 43002						in space
Phase 2 operational satellite in MEO for China's navigation satellite system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 6, 16:29	28246	0.0115	21542	22194	787.39	55.00	177
2017 Dec 7, 06:35	27906	0.0007	21508	21548	773.23	55.01	307
2023 Feb 12, 17:46	27906	0.0008	21505	21551	773.23	55.70	308
YZ-1 rocket stage 2017-069C 43003						in space
Launched Beidou-3 M-1 and M-2.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 6, 18:18	28657	0.0041	22160	22397	804.65	54.67	338
CZ 3B fourth stage 2017-069D 43004						Re-entered - 2021 Sep 22 Life 1417 days
Launched Beidou-3 M1 and M2.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 6, 18:18	15568	0.5793	172	18208	322.20	54.99	170

2017-070 Vega (VV-11) Centre Spatiale Guyanaise						2017 Nov 8, 01:42
Mohammed VI-A 2017-070A 43005						in space
Earth observation satellite from the Kingdom of Morocco to be used for mapping and land surveying to support regional development, agricultural monitoring, the prevention and management of natural disasters, and monitoring environment changes. It will also carry out border and coastal surveillance.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 8, 04:56	7000	0.0003	620	624	97.14	97.97	69	10:19
2017 Nov 12, 21:11	7007	0.0002	628	630	97.29	97.97	101	10:20
2017 Nov 16, 17:21	7017	0.0002	637	640	97.49	97.96	93	10:20
2023 Feb 13, 10:47	7017	0.0002	637	639	97.49	97.95	95	10:20
Vega upper stage uncatalogued						Re-entered - 2017 Nov 8 Life <1 day
Launched Mohammed VI-A. De-orbited shortly after satellite release, not catalogued.
Not Catalogued - orbit parameters unavailable

2017-071 Antares 230 Wallops Flight Facility						2017 Nov 12, 12:19
Cygnus OA-8E (SS Gene Cernan) 2017-071A 43006						Re-entered - 2017 Dec 18 Life 36 days
Cygnus resupply mission to ISS. Precise lift-off time 21:44:57 UTC. Captured by ISS remote arm Nov 14 at 10:04 UTC and docked with Unity module at approx12:15 UTC. Undocked 2016 Dec 5 at 17:52 UTC using the ISS remote Manipulator then released into independent orbit Dec 6 at 13:11 UTC. Cygnus released three batches of Cubesats later the same day and on Dec 7. It conducted other experiments in orbit. Retro-fire Dec 18 led to a destructive re-entry NE of New Zealand around at 12:54 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 12, 14:51	6639	0.0085	204	317	89.72	51.61	145
2017 Nov 14, 06:22	6783	0.0005	402	408	92.66	51.64	114
2017 Dec 5, 17:37	6783	0.0003	403	407	92.66	51.64	197
2017 Dec 6, 22:59	6830	0.0003	450	453	93.61	51.64	288
2017 Dec 9, 22:17	6769	0.0010	383	397	92.36	51.64	28
2017 Dec 14, 12:33	6767	0.0009	383	395	92.34	51.64	56
2017 Dec 16, 15:17	6762	0.0015	374	394	92.23	51.63	87
Lemur-2 (RocketJinah) 2017-071E 43041						Re-entered - 2022 Feb 14 Life 1555 days
3U Cubesat - equipped with a receiver for AIS (Automatic Information System) for tracking ships at sea, and other sensors. One of eight released from Cygnus OA-5 2016 Nov 25. Lemur-2 satellites are named after development and support team members. The is one of a cluster of eight Lemur-2 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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 20, 20:21	6830	0.0001	451	452	93.62	51.64	147
AeroCube 7B (OCSD - Optical Communications and Sensor Demonstration) 2017-071F 43042						Re-entered - 2022 Aug 5 Life 1727 days
1.5U Cubesat, separated from Aerocube 7C soon after being released by Cygnus. NASA funded mission to test LASER data transmission between satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 11, 00:55	6831	0.0005	450	457	93.65	51.64	323
AeroCube 7C (OCSD - Optical Communications and Sensor Demonstration) 2017-071G 43043						Re-entered - 2022 Aug 12 Life 1734 days
1.5U Cubesat, separated from Aerocube 7B soon after being released by Cygnus. NASA funded mission to test LASER data transmission between satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 11, 04:02	6831	0.0004	450	456	93.65	51.64	271
CHEFSat 1 (Cost-effective High E-Frequency Satellite) 2017-071H 43044						Re-entered - 2022 Jan 2 Life 1512 days
3U Cubesat testing the suitability of using commercial off-the-shelf radio frequency (RF) components and to better understand the effects of weather and atmospheric conditions on E-band links (30-300 GHz frequency).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 11, 14:57	6831	0.0005	450	456	93.65	51.64	312
Asgardia 1 2017-071N 43049						Re-entered - 2022 Sep 12 Life 1765 days
2U CubeSat tconducting a two-year radiation exposure test to measures data degradation on transmissions due to background noise from space radiation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 11, 02:27	6831	0.0006	448	456	93.64	51.64	177
ISARA (Integrated Solar Array & Reflectarray Antenna) 2017-071P 43050						Re-entered - 2022 Feb 23 Life 1564 days
3U Cubesat to verify aerial design and confirm 100 Mb/s is a viable data rate for transmission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 11, 04:01	6831	0.0001	452	453	93.64	51.64	229
PropCube 2 (Fauna) 2017-071R 43052						Re-entered - 2022 Jul 30 Life 1721 days
1U Cubesat studying irregularities in electron density and their effects on radio transmission.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 12, 19:00	6831	0.0002	451	454	93.64	51.64	342
MakerSat 1 2019-071M 45122						Re-entered - 2022 Oct 29 Life 1812 days
1U Cubesat (probably) developed by students at Northwest Nazarene University in Idaho to demonstrate satellite assembly on-orbit. Some components were 3D printed aboard the ISS. Released from Cygnus NG-12 Slingshot deployer, probably 2020 Feb 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2020 Feb 10, 20:24	6845	0.0010	460	473	93.93	51.64	285
Antares second stage 2017-071B 43007						Re-entered - 2017 Nov 25 Life 13 days
Launched SS Gene Cernan.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 12, 13:21	6658	0.0122	199	361	90.12	51.61	145

2017-072 CZ 4C Taiyuan Space Centre						2017 Nov 14, 18:35
Fengyun 3D (Fengyun 3-04) 2017-072A 43010						in space
Second generation meteorological imaging satellite capable of producing three-dimensional analyses of weather systems.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 15, 05:48	7183	0.0010	798	812	100.98	98.65	254	01:40
2017 Nov 24, 20:44	7205	0.0000	826	827	101.43	98.65	244	01:40
2023 Feb 13, 11:20	7206	0.0001	828	829	101.47	98.85	352	01:59
Head 1 2017-072B 43011						in space
Application satellite from Head Aerospace as a precursor to the Skywalker constellation, carrying a VDES, enhanced AIS receiver for ship-shore communications, and providing communications between internet-connected devices.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 15, 07:29	7181	0.0009	797	809	100.94	98.65	264	01:40
2023 Feb 13, 12:01	7180	0.0012	794	811	100.92	98.89	91	03:39
CZ 4C upper stage + Xinyun 2017-072C 43012						in space
Launched Fenyun 3D. Carries XInyun - a small, attached payload aimed at developing internet connectivity for objects in orbit. Perigee lowered after releasing satellites in order to hasten re-entry.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 14, 21:37	7084	0.0129	615	798	98.90	98.60	40

2017-073 Delta 7290-10C Vandenberg Air Force Base						2017 Nov 18, 09:47
NOAA 20 (JPSS, Joint Polar Satellite System 1) 2017-073A 43013						in space
US meteorological satellite belonging to the National Oceanographic and Atmospheric Agency measuring weather conditions in the Earth's atmosphere and providing weather images from polar orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 18, 14:25	7197	0.0002	817	820	101.27	98.71	107	01:25
2017 Dec 26, 22:54	7205	0.0001	826	828	101.44	98.71	68	01:25
2023 Feb 13, 13:29	7205	0.0002	826	828	101.44	98.74	82	01:25
Buccaneer RMM 2017-073B 43014						Re-entered - 2024 Oct 4 Life 2512 days
3U Cubesat designed for use in callibrating Jindalee Over-the-Horizon Radar Network (JORN), a military installation in northern Australia.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 19, 14:26	7018	0.0256	460	819	97.51	97.69	233
2023 Feb 12, 23:14	6971	0.0211	446	739	96.53	97.64	108
MiRaTA (Microwave Radiometer Technology Acceleration) 2017-073C 43015						in space
3U CubeSat from MIT's Lincoln Laboratory evaluating a suite of small instruments for Earth science missions.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 19, 16:03	7015	0.0258	456	818	97.46	97.69	233
2023 Feb 13, 10:48	6981	0.0226	445	760	96.74	97.65	106
MakerSat 0 2017-073D 43016						in space
1U Cubesat as technology proof-of-concept mission from NNU (Northwest Nazarene University) of Nampa, Idaho, USA, to demonstrate the characteristics of different plastics in the vacuum of space in preparation for MakerSat-1 – a CubeSat to be manufactured and assembled on the International Space Station. It also carries an imaging system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 19, 04:40	7015	0.0259	455	818	97.45	97.68	235
2023 Feb 13, 04:07	6990	0.0237	447	778	96.94	97.65	114
AO-91 2017-073E 43017						in space
1U Cubesat built by the AMSAT-North Amarica carrying a single-channel transponder for FM radio.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 19, 19:18	7015	0.0259	454	818	97.44	97.69	233
2023 Feb 13, 03:30	6995	0.0242	448	786	97.05	97.65	118
EagleSat 1 2017-073F 43018						in space
1U CubeSat built by the Embry-Riddle Aeronautical University to bring together its engineering disciplines that will test various types of memory for 'bit flipping' caused to solar radiation in low Earth orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 19, 17:40	7014	0.0259	455	818	97.44	97.69	233
2023 Feb 12, 22:56	6983	0.0229	445	765	96.79	97.65	109
Delta 4 upper stage uncatalogued						Re-entered - 2017 Nov 18 Life <1 day
Launched NOAA 20 and a collection of Cubesats. De-orbited soon after satellite separation, not catalogued.
Not Catalogued - orbit parameters unavailable

2017-I29 Nanoracks Cubesat Deployer International Space Station						2017 Nov 20, 08:05
EcAMSat (E.coli AntiMicrobial Satellite) 1998-067NG 43019						Re-entered - 2021 Dec 8 Life 1479 days
6U Cubesat (3x2) equipped with payload to investigate space microgravity effects on the antibiotic resistance of E.coli, a bacterial pathogen, as part of the Space Biology Project at NASA Ames Research Center.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 21, 09:43	6781	0.0006	399	407	92.62	51.64	113

2017-I30 Nanoracks Cubesat Deployer International Space Station						2017 Nov 20, 12:25
ASTERIA (Arcsecond Space Telescope Enabling Research in Astrophysics) 1998-067NH 43020						Re-entered - 2020 Apr 24 Life 886 days
6U Cubesat (3x2) using a telescope and camera to demonstrate precise pointing stability and repeatability from orbit-to-orbit. Joint a collaboration with the Massachusetts Institute of Technology and NASA JPL project.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 21, 09:41	6781	0.0003	401	405	92.62	51.64	110

2017-I31 Nanoracks Cubesat Deployer International Space Station						2017 Nov 20, 17:02
Dellingr (Radiation Belt Loss Experiment) 1998-067NJ 43021						Re-entered - 2021 Jun 10 Life 1298 days
6U Cubesat (3x2) from NASA to gather high-quality data about the Sun’s influence on Earth’s upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 20, 22:38	6781	0.0003	401	405	92.62	51.64	100

2017-074 CZ 6 (Y-2) Taiyuan Space Centre						2017 Nov 21, 04:50
Jilin-1 Smart Video 04 (Jilin-1 SP04) 2017-074A 43022						in space
Chinese commercial imaging satellite providing high definition Earth surface video. Part of a simultaneously-launched Jilin-1 cluster of three satellites, named after the city where the satellites were developed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 21, 12:16	6917	0.0010	532	546	95.42	97.54	266	12:00
2017 Dec 6, 22:08	6919	0.0011	533	548	95.45	97.54	193	11:59
2023 Feb 13, 13:53	6905	0.0008	522	533	95.17	97.50	164	11:35
Jilin-1 Smart Video 05 (Jilin-1 SP05) 2017-074B 43023						in space
Chinese commercial imaging satellite providing high definition Earth surface video. Part of a simultaneously-launched Jilin-1 cluster of three satellites, named after the city where the satellites were developed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 21, 15:27	6916	0.0010	532	545	95.41	97.54	265	12:00
2017 Dec 6, 20:08	6914	0.0011	528	543	95.35	97.54	205	11:59
2023 Feb 13, 13:35	6905	0.0008	521	532	95.16	97.50	179	11:36
Jilin-1 Smart Video 06 (Jilin-1 SP06) 2017-074C 43024						in space
Chinese commercial imaging satellite providing high definition Earth surface video. Part of a simultaneously-launched Jilin-1 cluster of three satellites, named after the city where the satellites were developed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Nov 21, 15:27	6916	0.0010	531	545	95.41	97.54	268	12:00
2017 Dec 6, 22:00	6916	0.0010	531	545	95.40	97.54	209	11:59
2023 Feb 13, 12:32	6906	0.0010	520	535	95.18	97.50	183	11:36
CZ 6 third stage 2017-074D 43025						Re-entered - 2023 Nov 11 Life 2181 days
Launch Jilin cluster. Perigee lowered after releasing satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 21, 15:27	6842	0.0102	394	534	93.87	97.54	26

2017-I32 Nanoracks Cubesat Deployer International Space Station						2017 Nov 21, 08:25
TechEdSat 6 1998-067NK 43026						Re-entered - 2018 May 15 Life 175 days
3.5U Cubesat from NASA fitted with Exo-Brake, resembling a configurable, cross-shaped parachute capable of varying its drag to control re-entry.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 22, 19:03	6780	0.0002	400	403	92.59	51.64	80

2017-I33 Nanoracks Cubesat Deployer International Space Station						2017 Nov 21, 11:40
OSIRIS-3U 1998-067NL 43027						Re-entered - 2019 Mar 7 Life 471 days
3U Cubesat developed by Penn State University to study space weather phenomena created by stimulating the ionosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 22, 07:14	6780	0.0005	399	405	92.60	51.64	90

2017-075 CZ 2C Xichang Space Centre						2017 Nov 24, 18:10
Yaogan 30-02A 2017-075A 43028						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 25, 00:24	6975	0.0010	590	604	96.62	35.00	293
2017 Dec 26, 01:11	6978	0.0003	598	601	96.68	34.99	285
2023 Feb 13, 09:42	6972	0.0001	592	594	96.55	35.00	148
Yaogan 30-02B 2017-075B 43029						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 25, 08:09	6975	0.0010	590	604	96.62	35.00	293
2017 Dec 16, 10:36	6978	0.0004	597	603	96.68	34.99	114
2023 Feb 13, 10:48	6972	0.0004	590	596	96.55	35.00	89
Yaogan 30-02C 2017-075C 43030						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 25, 12:58	6975	0.0010	590	604	96.62	35.00	296
2017 Dec 20, 20:14	6978	0.0004	597	603	96.68	34.99	327
2023 Feb 13, 10:15	6971	0.0004	590	596	96.55	35.00	285
CZ 2C second stage 2017-075D 43031						in space
Launched cluster of three Yaogan-30 satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Nov 25, 22:13	6906	0.0103	456	599	95.18	35.21	63

2017-F05 - failed to reach orbit Soyuz-2.1b + Fregat Vostochny Cosmodrome						2017 Nov 28, 05:41
Multiple satellites
Group of 19 satellites lost due to launch software being incorrectly programmed. Satellites carried were Russia's Meteor M2-1 meteorological satellite, Telesat Canada's LEO 2 comsat, AISSat 3 from Norway, Baumanets 2 - a remote sensing satellite, IDEA OSG - a space debris detector, two Corvus BC imaging satellites, ten Lemur-2 satellites, SEAM - a Swedish satellite to study aurorae and radio waves, and the D-Star 1 comsat.

2017-076 Soyuz-2.1b Plesetsk Cosmodrome						2017 Dec 2, 10:43
Cosmos 2524 (Lotos-S1 № 2) 2017-076A 43032						in space
Electronic intelligence gathering - signals intelligence (SIGINT) satellite. Vehicle is based on the design of the Yantar satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 3, 07:48	6948	0.0476	239	901	96.06	67.14	92
2017 Dec 8, 13:07	7283	0.0006	901	910	103.10	67.15	267
Soyuz upper stage 2017-076B 43033						Re-entered - 2019 May 15 Life 529 days
Launched Cosmos 2524.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 2, 20:34	6938	0.0463	238	881	95.85	67.14	92

2017-077 CZ 2D Jiuquan Space Centre						2017 Dec 3, 04:11
LKW 1 (Land Survey Satellite 1) 2017-077A 43034						in space
High resolution imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Dec 3, 18:32	6874	0.0010	489	503	94.54	97.46	256	10:30
2023 Feb 13, 02:08	6874	0.0002	494	497	94.53	97.27	147	10:03
CZ 2D second stage uncatalogued						Re-entered - 2017 Dec 3 Life <1 day
Launched LKW 1. De-orbited shortly after satellite separation, not catalogued.
Not Catalogued - orbit parameters unavailable

2017-078 CZ 3B Xichang Space Centre						2017 Dec 10, 16:40
Alcomsat 1 2017-078A 43039						in space
Chines built comsat for Algeria. Expected location 24°.8 west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	GEO     Longitude
2017 Dec 11, 10:42	27366	0.7604	180	41795	750.88	26.36	180
2017 Dec 22, 18:42	42164	0.0002	35776	35796	1436.07	0.05	81	24°.8 W
2023 Feb 12, 09:26	42165	0.0003	35775	35799	1436.11	0.04	161	24°.8 W
CZ 3B fourth stage 2017-078B 43040						Re-entered - 2018 Mar 10 Life 90 days
Launched Alcomsat 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 11, 04:44	26470	0.7537	142	40043	714.33	26.38	179

2017-079 Ariane 5ES (VA-240) Centre Spatiale Guyanaise						2017 Dec 12, 18:36
Galileo 19 (Nicole, Galileo FOC FM-15) 2017-079A 43055						in space
One of a group of quadruple-launched Galileo FOC (Full Operation Capacity) satellites for the European Space Agency navigation system. Also carries a COSPAS-SARSAT search and rescue receiver to detect distress signals from the Earth's surface.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 15, 00:15	29305	0.0008	22905	22949	832.10	57.02	222
2017 Dec 17, 19:20	29455	0.0032	22983	23170	838.47	56.94	206
2017 Dec 20, 00:23	29552	0.0004	23162	23186	842.63	56.99	322
2017 Dec 30, 04:08	29685	0.0003	23298	23316	848.34	56.98	230
2018 Feb 1, 19:55	29600	0.0001	23220	23224	844.69	56.98	85
Galileo 20 (Zofia, Galileo FOC FM-16) 2017-079B 43056						in space
One of a group of quadruple-launched Galileo FOC (Full Operation Capacity) satellites for the European Space Agency navigation system. Also carries a COSPAS-SARSAT search and rescue receiver to detect distress signals from the Earth's surface.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 15, 04:06	29294	0.0004	22904	22928	831.64	57.01	253
2017 Dec 28, 00:00	29556	0.0002	23171	23183	842.79	56.92	334
2018 Feb 2, 15:02	29601	0.0004	23212	23234	844.74	56.95	270
Galileo 21 (Alexandre, Galileo FOC FM-17) 2017-079C 43057						in space
One of a group of quadruple-launched Galileo FOC (Full Operation Capacity) satellites for the European Space Agency navigation system. Also carries a COSPAS-SARSAT search and rescue receiver to detect distress signals from the Earth's surface.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 14, 14:56	29290	0.0002	22906	22918	831.47	56.94	239
2017 Dec 28, 00:00	29463	0.0004	23073	23096	838.81	56.94	88
2018 Feb 16, 12:58	29527	0.0024	23078	23220	841.57	56.97	340
2018 Mar 1, 19:37	29600	0.0002	23216	23229	844.71	56.93	295
Galileo 22 (Irina, Galileo FOC FM-18) 2017-079D 43058						in space
One of a group of quadruple-launched Galileo FOC (Full Operation Capacity) satellites for the European Space Agency navigation system. Also carries a COSPAS-SARSAT search and rescue receiver to detect distress signals from the Earth's surface.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 14, 14:49	29284	0.0003	22897	22914	831.19	57.02	196
2017 Dec 21, 12:13	29405	0.0042	22903	23150	836.34	56.96	13
2017 Dec 25, 03:46	29534	0.0002	23150	23161	841.85	56.98	271
2018 Feb 21, 09:52	29600	0.0003	23213	23231	844.70	56.94	277
Ariane 5 upper stage 2017-079E 43059						in space
Launched cluster of Galileo satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 14, 14:57	29278	0.0002	22893	22906	830.93	57.02	17

2017-080 Falcon 9 v1.2 Cape Canaveral Air Force Station						2017 Dec 15, 15:36
SpaceX Dragon CRS-13 2017-080A 43060						Re-entered - 2018 Jan 13 Life 29 days Returned to Earth
Carrying a cargo to the ISS under NASA's Commercial Resupply Services (CRS) contract. Captured by the ISS Remote Manipulator System Dec 17 at 10:57 UTC and attached to the lower port of the Harmony module at 13:26 UTC. Undocked using the RMS 2018 Jan 12 at 10:47 UTC. Released Jan 13 at 09:58 UTC. Retro-fire led to splashdown at 15:37 UTC in the Pacific Ocean, about 300 km SW of Baja, California.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 15, 18:52	6657	0.0114	204	355	90.10	51.64	46
2017 Dec 16, 20:03	6762	0.0119	303	464	92.23	51.76	165
Falcon 9 upper stage uncatalogued						Re-entered - 2017 Dec 15 Life <1 day
Launched SpaceX Dragon CRS-13. De-orbited shortly after spacecraft separation, not Catalogued.
Not Catalogued - orbit parameters unavailable

2017-081 Soyuz-FG 11A511U-FG Baikonur Cosmodrome						2017 Dec 17, 07:21
Soyuz MS-07 (Soyuz 11F732A48 № 737) 2017-081A 43063						Re-entered - 2018 Jun 3 Life 168 days Returned to Earth
Carrying crew to ISS - Anton Shkaplerov (Roscosmos), Scott Tingle (NASA) and Norishige (Japan). Docked with the Rassvet module of the ISS Dec 19 at 08:39 UTC, four minutes earlier than planned. Undocked, carrying its original crew, 2018 Apr 3 at 09:14:40 UTC. Retro-fire at 11:47 UTC was followd by landing in Kazakhstan, 147 kilometers south east of Dzhezkazgan, at 12:39 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 17, 16:24	6635	0.0010	250	263	89.64	51.64	134
2017 Dec 19, 07:34	6783	0.0003	403	406	92.65	51.64	257
Soyuz upper stage 2017-081B 43064						Re-entered - 2017 Dec 20 Life 3 days
Launched Soyuz MS-07.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 17, 07:52	6586	0.0027	190	226	88.65	51.62	60

2017-082 H-IIA 202 (F-37) Tanegashima Space Centre						2017 Dec 23, 01:26
Shikisai (GCOM-C) 2017-082A 43065						in space
Global Change Observation Mission, an imaging satellite monitoring changes in aerosols, cloud cover and vegetation
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Dec 23, 15:59	7170	0.0002	790	793	100.70	98.70	188	10:15
2018 Jan 22, 13:41	7179	0.0001	800	802	100.89	98.68	114	10:16
2023 Feb 13, 05:08	7179	0.0001	800	802	100.89	98.62	99	10:26
Tsubame (Super Low Altitude Test Satellite) 2017-082B 43066						Re-entered - 2019 Oct 1 Life 647 days
Small satellite from the Tokyo Institute of Technolgy observing ephemeral, high-energy phenomena, such as gamma ray bursts, using polarimetry of hard X-rays. Also acted as demostrator for a new gyro system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 08:56	6921	0.0124	457	629	95.51	98.32	110
H-2A upper stage 2017-082C 43067						in space
Launched GCOM-C and Tsubame.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 05:45	6927	0.0127	461	637	95.63	98.34	113

2017-083 Falcon 9 v1.2 Vandenberg Air Force Base						2017 Dec 23, 01:27
Iridium 135 (Iridium Next) 2017-083A 43070						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 08:57	6997	0.0011	611	627	97.08	86.69	264
2018 Mar 5, 08:39	7156	0.0003	776	780	100.40	86.40	86
Iridium 138 (Iridium Next) 2017-083B 43071						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 08:57	6997	0.0012	611	627	97.08	86.69	269
2018 Mar 5, 14:17	7156	0.0002	776	779	100.40	86.40	102
Iridium 116 (Iridium Next) 2017-083C 43072						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 08:57	6997	0.0011	611	626	97.08	86.69	256
2018 Mar 5, 18:33	7156	0.0002	776	779	100.40	86.40	88
Iridium 130 (Iridium Next) 2017-083D 43073						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 08:57	6997	0.0011	611	626	97.08	86.69	255
2018 Mar 5, 14:26	7156	0.0002	776	779	100.40	86.40	99
Iridium 151 (Iridium Next) 2017-083E 43074						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 08:57	6997	0.0011	611	626	97.07	86.69	254
2018 Mar 5, 08:48	7156	0.0002	776	779	100.40	86.40	86
Iridium 134 (Iridium Next) 2017-083F 43075						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 08:57	6996	0.0012	610	626	97.06	86.69	256
2018 Mar 5, 14:44	7156	0.0003	776	779	100.40	86.40	100
Iridium 137 (Iridium Next) 2017-083G 43076						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 08:56	6996	0.0012	610	626	97.06	86.68	254
2018 Mar 5, 20:04	7156	0.0002	776	779	100.40	86.40	82
Iridium 141 (Iridium Next) 2017-083H 43077						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 08:56	6996	0.0011	610	626	97.06	86.68	251
2018 Mar 5, 14:53	7156	0.0002	776	779	100.40	86.40	99
Iridium 153 (Iridium Next) 2017-083J 43078						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 08:56	6996	0.0011	610	626	97.05	86.69	253
2018 Sep 7, 12:08	7156	0.0002	776	779	100.40	86.40	56
Iridium 131 (Iridium Next) 2017-083K 43079						in space
One of a simultaneously-launched set of ten satellites. Will replace a satellite in the first generation Iridium constellation providing satellite-based voice and data telephony services.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 23, 08:56	6996	0.0012	609	626	97.05	86.68	256
2018 Mar 5, 14:35	7156	0.0002	776	779	100.40	86.40	102
Falcon 9 upper stage uncatalogued						Re-entered - 2017 Dec 23 Life <1 day
Launched cluster of Iridium satellites. De-orbited shortly after satellite separation, not catalogued.
Not Catalogued - orbit parameters unavailable

2017-084 CZ 2D Jiuquan Space Centre						2017 Dec 23, 04:14
LKW-2 (Land Survey Satellite 2) 2017-084A 43080						in space
High resolution imaging satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )	Desc Node Local Time
2017 Dec 23, 13:40	6874	0.0009	490	503	94.54	97.46	261	10:33
2023 Feb 13, 09:17	6873	0.0002	493	497	94.52	97.28	148	10:11
CZ 2D second stage uncatalogued						Re-entered - 2017 Dec 23 Life <1 day
Launched LKW-1. De-orbited shortly after satellite separation, not catalogued.
Not Catalogued - orbit parameters unavailable

2017-085 CZ 2C Xichang Space Centre						2017 Dec 25, 19:44
Yaogan 30-03A 2017-085A 43081						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 26, 03:42	6975	0.0010	590	603	96.62	35.00	290
2018 Jan 1, 08:45	6969	0.0007	585	596	96.49	35.00	301
2018 Jan 14, 01:54	6978	0.0001	599	600	96.68	35.02	328
2023 Feb 13, 04:44	6971	0.0005	590	597	96.55	35.00	345
Yaogan 30-03B 2017-085B 43082						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 26, 05:21	6975	0.0010	590	604	96.62	35.00	292
2018 Jan 14, 13:41	6978	0.0005	596	603	96.68	35.00	121
2023 Feb 13, 05:16	6971	0.0005	590	597	96.55	35.00	218
Yaogan 30-03C 2017-085C 43083						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 )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 26, 05:25	6975	0.0008	591	603	96.62	35.00	290
2017 Dec 31, 22:04	6984	0.0007	602	611	96.82	34.99	285
2018 Jan 2, 04:12	6986	0.0005	604	611	96.84	35.00	290
2018 Jan 17, 14:37	6978	0.0006	596	604	96.68	35.00	277
2023 Feb 13, 10:36	6972	0.0006	589	598	96.55	35.00	345
CZ 2C second stage 2017-085D 43084						in space
Launched cluster of three Yaogan-30 satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 26, 03:33	6933	0.0103	483	626	95.75	34.67	344

2017-086 Zenit-3SLB + Fregat Baikonur Cosmodrome						2017 Dec 26, 19:00
Angosat 1 (Angosat № 1L) 2017-086A 43087						in space
Russian built comsat to be operated by Angosat of Angola. Stranded in geosynchronous drift orbit when a power problem prevented proper communication with ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 31, 18:39	42418	0.0018	35962	36118	1449.06	0.07	98
2023 Feb 12, 12:02	42415	0.0016	35971	36104	1448.92	4.49	143
Fregat rocket stage 2017-086B 43088						in space
Launched Angosat 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 31, 15:27	42701	0.0105	35875	36770	1463.57	0.21	36
Zenit upper stage 2017-086D 43090						Re-entered - 2018 Jan 27 Life 32 days
Launched Angosat 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl  ( ° )	ω   ( ° )
2017 Dec 27, 05:29	6735	0.0283	166	547	91.67	51.37	60