2014 - Satellite & Spacecraft Launches and Detailed Orbits

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2014-001 GSLV MK II D5 Satish Dhawan Space Centre						2014 Jan 5, 10:48
GSat 14 2014-001A 39498						in space
Indian comsat, replacement for GSat 3. Expected location - 74° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Jan 5, 16:30	24347	0.7314	160	35777	630.13	19.41	178
2014 Jan 6, 14:01	28733	0.4668	8943	35767	807.84	7.60	178
2014 Jan 7, 06:09	40521	0.0395	32544	35741	1352.92	0.67	162
2014 Jan 13, 03:08	41984	0.0032	35471	35742	1426.89	0.26	129
2014 Jan 17, 00:25	42081	0.0018	35627	35779	1431.84	0.25	124	73°.5 E
2014 Jan 26, 18:41	42165	0.0006	35763	35810	1436.10	0.23	26	74°.0 E
2023 Feb 13, 11:43	42165	0.0005	35765	35808	1436.09	0.10	19	74°.0 E

2014-002 Falcon 9 v1.1 Cape Canaveral Air Force Station						2014 Jan 6, 22:06
Thaicom 6 2014-002A 39500						in space
Comsat to serve the mainland of south east Asia, particularly Thailand. Some services will be provided to east Africa, including Madagascar. Time was the opening of a 26-27 minute window. Launch postponed from Dec 19 and Jan 3. Will be co-located with Thaicom 5. Expected location - 78º.5 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Jan 6, 23:43	53191	0.8705	510	93117	2034.80	22.46	181
2014 Jan 9, 19:45	58365	0.6564	13674	90299	2338.75	6.88	180
2014 Jan 15, 13:23	46030	0.0814	35904	43400	1638.03	0.35	186
2014 Jan 17, 20:13	43294	0.0236	35895	37936	1494.15	0.13	201
2014 Jan 21, 21:13	42201	0.0007	35795	35852	1437.97	0.05	127	78°.6 E
2014 Jan 22, 10:50	42165	0.0001	35783	35791	1436.11	0.05	105	78°.4 E
2023 Feb 13, 13:14	42165	0.0001	35784	35790	1436.10	0.05	247	78°.5 E

2014-003 Antares 120 Wallops Flight Facility						2014 Jan 9, 18:07
Orb 1 (SS C Gordon Fullerton) 2014-003A 39502						Re-entered - 2014 Feb 19 Life 41 days
Cargo delivery mission under the NASA Commercial Orbital Transportation Services (COTS) agreement. The Cygnus pressurized cargo vessel is based the on the Multi-Purpose Logistics Module (MPLM) carried as Shuttle cargo, and the avionics have been developed for other satellites. Carried the Nanoracks CM3 cubesat cluster, for launch from the ISS, consisting of 28 satellites of the Planet Labs Flock 1A, SkyCube ArduSat-2), LithuanicaSat, LitSat, and UAPSat. Cygnus was captured by the ISS Remote Manipulator 2014 Jan 12 at 11:08 UTC and docked with the downward-facing port of Unity at 13:05 UTC. Undocked Feb 18 at 10:04 UTC and released from the Remote Manipulator at 11:31 UTC. Retro-fire Oct 23 at 17:41 UTC led to a destructive re-entry at 18:16 UTC with any surviving fragments hitting the surface of the southern Pacific Ocean 20-30 minutes later.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jan 9, 22:29	6620	0.0028	223	261	89.34	51.62	142
2014 Jan 10, 20:21	6790	0.0005	408	415	92.80	51.64	23
2014 Jan 12, 09:12	6794	0.0006	412	420	92.88	51.65	20

2014-004 Atlas V 401, AV-043 Cape Canaveral Air Force Station						2014 Jan 24, 02:33
TDRS 12 (Tracking and Data Relay Satellite) 2014-004A 39504						in space
Part of the next-generation series in the Tracking and Data Relay Satellite System, providing tracking, telemetry, command and high-bandwidth data relay from satellites and spacecraft in orbit. Launch was within a 45 minute window that opened at 02:05 UTC. Renamed from TDRS-L 2014 October.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Jan 24, 20:55	26694	0.5797	4842	35790	723.41	25.45	180
2014 Jan 27, 18:00	29405	0.4341	10262	35791	836.34	17.86	181
2014 Feb 17, 06:37	42165	0.0001	35782	35791	1436.09	6.99	327	149°.7 W
2023 Feb 13, 09:27	42166	0.0001	35786	35790	1436.17	3.68	57	41°.0 W

2014-005 Soyuz-FG 11A511U-FG Baikonur Cosmodrome						2014 Feb 5, 16:23
Progress M-22M (Progress 7K-TGM №422) 2014-005A 39506						Re-entered - 2014 Apr 18 Life 72 days
Supplies to ISS. Precise launch time - 16:23:32 UTC. Docked automatically with the port on Pirs at 22:22 UTC, about three minutes earlier than anticipated. Undocked 2014 Apr 7 at 13:58:22 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 5, 16:12	6587	0.0031	188	229	88.67	51.62	83
2014 Feb 5, 18:28	6713	0.0024	319	351	91.24	51.63	78
2014 Feb 6, 14:12	6795	0.0004	414	419	92.90	51.65	110

2014-006 Ariane 5ECA (VA-217) Centre Spatiale Guyanaise						2014 Feb 6, 21:30
ABS 2 (Asia Broadcast Satellite 2) 2014-006A 39508						in space
Comsat including broadcasting for direct-to-home and cable television distribution, VSAT (very-small-aperture terminal) services, data networks and telecommunications. Coverage - Middle East, Africa, Russia and the Asia-Pacific region. Design life 15 years minimum. Expected location - 75° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Feb 7, 19:16	24393	0.7281	255	35775	631.93	6.02	179
2014 Feb 8, 05:51	26486	0.5909	4457	35759	714.97	3.76	179
2014 Feb 10, 18:40	34766	0.2119	21021	35754	1075.20	0.79	182
2014 Feb 19, 16:48	42163	0.0002	35778	35793	1436.03	0.08	51	74°.7 E
2023 Feb 12, 19:07	42165	0.0003	35774	35799	1436.10	0.06	29	74°.9 E

Athena-Fidus 2014-006B 39509						in space
'Access on THeatres for European Nations Allied forces' - French Italian Dual Use Satellite - funded jointly by CNES, French defense procurement agency DGA, Italian space agency ASI and the Italian Ministry of Defense to provide services to both armed forces and civil security agencies in France and Italy. Expected location - 25° east. No orbit data has been made available to show the move between GTO and the initial GEO location.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Feb 7, 15:15	24373	0.7281	250	35739	631.13	6.03	179
2014 Feb 26, 15:40	42164	0.0000	35784	35788	1436.06	0.05	58	37°.8 E
2015 Oct 27, 19:05	42164	0.0001	35782	35791	1436.08	0.03	319	37°.9 E
2023 Feb 12, 13:10	42165	0.0002	35780	35793	1436.09	0.01	195	37°.8 E

2014-I01 Nanoracks Cubesat Deployer International Space Station						2014 Feb 11, 08:33
Flock 1A-1 1998-067DH 39513						Re-entered - 2014 Jun 9 Life 118 days
3U Cubesat, part of Planet Labs "Flock 1a", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Release delayed from Feb 6. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 12, 07:58	6792	0.0004	412	417	92.85	51.64	148

Flock 1A-2 1998-067DJ 39514						Re-entered - 2014 May 25 Life 103 days
3U Cubesat, part of Planet Labs "Flock 1A", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Release delayed from Feb 6. Name/designation are as listed by SpaceTrack. Solar panel deployed around February 25.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 12, 08:00	6792	0.0005	411	417	92.85	51.65	165

2014-I02 Nanoracks Cubesat Deployer International Space Station						2014 Feb 11, 12:41
Flock 1A-3 1998-067DG 39512						Re-entered - 2014 May 15 Life 93 days
3U Cubesat, part of Planet Labs "Flock 1A", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Release delayed from Feb 6. Name/designation are as listed by SpaceTrack - Planet Labs has issued at least two alternative versions. Solar panel deployed around February 21.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 12, 07:57	6792	0.0006	410	419	92.85	51.65	119

Flock 1A-4 1998-067DK 39515						Re-entered - 2014 Jun 18 Life 127 days
3U Cubesat, part of Planet Labs "Flock 1A", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Release delayed from Feb 6. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 12, 08:00	6792	0.0006	410	418	92.85	51.65	117

2014-I03 Nanoracks Cubesat Deployer International Space Station						2014 Feb 12, 08:30
Flock 1A-5 1998-067DL 39518						Re-entered - 2014 Jun 2 Life 110 days
3U Cubesat, part of Planet Labs "Flock 1A", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 13, 08:48	6792	0.0009	408	420	92.85	51.63	62

Flock 1A-6 1998-067DM 39519						Re-entered - 2014 Jun 15 Life 123 days
3U Cubesat, part of Planet Labs "Flock 1A", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 13, 08:48	6792	0.0008	408	420	92.85	51.64	62

2014-I04 Nanoracks Cubesat Deployer International Space Station						2014 Feb 13, 08:20
Flock 1A-7 1998-067DN 39520						Re-entered - 2014 Jun 5 Life 112 days
3U Cubesat, part of Planet Labs "Flock 1A", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack - Planet Labs has issued at least two alternative versions. Solar panel deployed around March 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 14, 01:40	6792	0.0007	410	419	92.85	51.65	160

Flock 1A-8 1998-067DP 39521						Re-entered - 2014 May 25 Life 101 days
3U Cubesat, part of Planet Labs "Flock 1A", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack - Planet Labs has issued at least two alternative versions. Solar panel deployed around March 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 14, 01:42	6792	0.0007	409	419	92.85	51.65	163

2014-I05 Nanoracks Cubesat Deployer International Space Station						2014 Feb 14, 04:10
Flock 1A-9 1998-067DQ 39525						Re-entered - 2014 Jul 6 Life 142 days
3U Cubesat, part of Planet Labs "Flock 1A", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack - Planet Labs has issued at least two alternative versions. Solar panel deployed around March 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 15, 04:06	6792	0.0007	409	418	92.85	51.65	143

Flock 1A-10 1998-067DR 39526						Re-entered - 2014 Jun 14 Life 120 days
3U Cubesat, part of Planet Labs "Flock 1A", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack - Planet Labs has issued at least two alternative versions. Solar panel deployed around March 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 15, 04:06	6792	0.0006	410	418	92.85	51.65	143

2014-I06 Nanoracks Cubesat Deployer International Space Station						2014 Feb 14, 04:15
Flock 1A-11 1998-067DS 39527						Re-entered - 2014 Jun 13 Life 119 days
3U Cubesat, part of Planet Labs "Flock 1A", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack - Planet Labs has issued at least two alternative versions. Solar panel deployed around March 13.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 15, 20:59	6792	0.0006	409	418	92.84	51.65	117

Flock 1A-12 1998-067DT 39528						Re-entered - 2014 Oct 26 Life 254 days
3U Cubesat, part of Planet Labs "Flock 1A", consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack - Planet Labs has issued at least two alternative versions. Failed both to stabilise itself and deploy solar panels.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 15, 21:03	6792	0.0006	410	418	92.85	51.65	121

2014-007 Proton-M + Briz-M Baikonur Cosmodrome						2014 Feb 14, 21:09
Türksat 4A 2014-007A 39522						in space
Comsat to provide direct TV broadcasting communications channels to Turkey, Europe, Central Asia, the Middle East and Africa. First three orbits listed are estimates based on data from Khrunichev. Separated from Briz-M Feb 15 at 06:21 UTC. Expected location - 50° east where it will operate until Türksat 4B arrives late-2014. It will then move to 42° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Feb 14, 21:25	6550	0.0001	171	172	87.92	51.57	100
2014 Feb 14, 22:34	9013	0.2624	270	5000	141.93	50.33	358
2014 Feb 15, 00:56	24415	0.7222	404	35670	632.77	49.10	359
2014 Feb 15, 12:56	29107	0.4485	9676	35783	823.69	12.69	360
2014 Feb 18, 08:02	40993	0.0285	33448	35781	1376.65	0.47	2
2014 Feb 20, 21:37	42084	0.0017	35633	35780	1431.99	0.01	357	49°.1 E
2014 Feb 24, 02:35	42165	0.0002	35776	35797	1436.08	0.01	241	50°.0 E
2014 Jun 5, 16:31	42243	0.0002	35855	35875	1440.12	0.07	163
2014 Jun 16, 22:49	42168	0.0000	35789	35790	1436.25	0.07	21	41°.8 E
2015 Oct 26, 18:52	42165	0.0005	35768	35807	1436.12	0.03	325	42°.0 E
2023 Feb 13, 07:41	42165	0.0004	35769	35804	1436.09	0.06	30	42°.0 E

2014-I07 Nanoracks Cubesat Deployer International Space Station						2014 Feb 15, 07:00
Flock 1A-13 1998-067DU 39529						Re-entered - 2014 Jul 2 Life 137 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Release delayed from Feb 13 when NanoRacks deployer failed to operate. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack - Planet Labs has issued at least two alternative versions. Solar panel deployed around March 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 16, 04:52	6792	0.0002	412	416	92.85	51.65	180

Flock 1A-14 1998-067DV 39530						Re-entered - 2014 Jun 20 Life 125 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Release delayed from Feb 13 when NanoRacks deployer failed to operate. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack - Planet Labs has issued at least two alternative versions. Solar panel deployed around March 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 16, 03:17	6792	0.0003	412	416	92.85	51.65	187

2014-I08 Nanoracks Cubesat Deployer International Space Station						2014 Feb 15, 10:55
Flock 1A-15 1998-067DW 39531						Re-entered - 2014 May 21 Life 95 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Release delayed from Feb 13 when NanoRacks deployer failed to operate. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack - Planet Labs has issued at least two alternative versions. Solar panel deployed around March 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 16, 04:43	6792	0.0006	410	418	92.84	51.65	113

Flock 1A-16 1998-067DX 39532						Re-entered - 2014 Jun 20 Life 125 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Release delayed from Feb 13 when NanoRacks deployer failed to operate. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack - Planet Labs has issued at least two alternative versions. Solar panel deployed around March 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 16, 04:52	6792	0.0006	410	418	92.85	51.65	126

2014-008 Delta 4 Medium+ 4,2 Cape Canaveral Air Force Station						2014 Feb 21, 01:59
USA 248 (Navstar GPS IIF-05) 2014-008A 39533						in space
Fifth Block 2F, Generation 2 GPS Navsat. Postponement from Oct 23 announced on Oct 16 - resulted from ongoing investigation into Delta 4 engine anomaly during the GPS IIF-03 launch 2012 October. Launch delayed 19 mins to end of window in order to move trajectory away from an area of high solar radiation. Separated from launch vehicle at 05:32:05 UTC. The first two listed orbits are estimates based on data provided by ULA Launch and were while USA 248 was still attached to the launch vehicle upper stage.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 21, 02:11	6678	0.0172	185	414	90.51	41.60	120
2014 Feb 22, 16:25	26841	0.0002	20457	20469	729.39	54.98	223

2014-I09 Nanoracks Cubesat Deployer International Space Station						2014 Feb 25, 17:20
Flock 1A-17 1998-067DY 39555						Re-entered - 2014 May 19 Life 83 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 27, 02:16	6791	0.0006	408	417	92.82	51.65	119

Flock 1A-18 1998-067DZ 39556						Re-entered - 2014 Oct 29 Life 246 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Failed both to stabilise itself and deploy solar panels.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 27, 03:49	6791	0.0005	409	416	92.82	51.64	119

2014-I10 Nanoracks Cubesat Deployer International Space Station						2014 Feb 26, 04:20
Flock 1A-19 1998-067EC 39559						Re-entered - 2014 Jun 3 Life 97 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 11:58	6790	0.0005	409	416	92.81	51.65	231

Flock 1A-20 1998-067ED 39560						Re-entered - 2014 Oct 9 Life 225 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Failed both to stabilise itself and deploy solar panels.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 10:23	6791	0.0005	409	416	92.82	51.64	224

2014-I11 Nanoracks Cubesat Deployer International Space Station						2014 Feb 26, 07:35
Flock 1A-21 1998-067EA 39557						Re-entered - 2014 May 25 Life 88 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 10:23	6791	0.0007	407	417	92.81	51.64	195

Flock 1A-22 1998-067EB 39558						Re-entered - 2014 Jun 4 Life 98 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 27, 03:50	6791	0.0007	408	417	92.82	51.65	202

2014-I12 Nanoracks Cubesat Deployer International Space Station						2014 Feb 27, 01:50
Flock 1A-23 1998-067EE 39561						Re-entered - 2014 Jul 10 Life 133 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 27, 23:40	6791	0.0007	408	418	92.83	51.66	167

Flock 1A-24 1998-067EF 39562						Re-entered - 2014 Jun 16 Life 109 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 27, 22:08	6791	0.0020	400	426	92.83	51.64	172

2014-I13 Nanoracks Cubesat Deployer International Space Station						2014 Feb 27, 07:40
Flock 1A-25 1998-067EG 39563						Re-entered - 2014 Jun 24 Life 117 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 18.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 27, 19:05	6791	0.0004	409	415	92.81	51.65	153

Flock 1A-26 1998-067EH 39564						Re-entered - 2014 Jun 10 Life 103 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Name/designation are as listed by SpaceTrack. Solar panel deployed around March 23.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 27, 20:42	6791	0.0005	409	416	92.82	51.65	156

2014-009 H-IIA 202 (F-23) Tanegashima Space Centre						2014 Feb 27, 18:37
ShindaiSat 2014-009A 39572						Re-entered - 2014 Nov 24 Life 270 days
Demonstrator satellite equipped with an LED to drive an optical communications ground station link at distances up to 400 kilometres.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 13:13	6770	0.0012	384	401	92.40	65.01	284

ITF 1 (Image The Future 1) 2014-009B 39573						Re-entered - 2014 Jun 29 Life 122 days
1U CubeSat for the University of Tsukuba, Japan that will transmit data to simple receivers by the use of Morse Code.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 13:04	6765	0.0008	381	392	92.28	65.02	347

GPM Core (Global Precipitation Measurement mission - Core satellite) 2014-009C 39574						in space
Joint between NASA and JAXA. The GPM Core observatory is equipped with radar and microwave imagers to collect data to measure precipitation in the Earth's atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 11:06	6775	0.0012	388	405	92.49	65.02	257

OPUSat (Osaka Prefecture University Satellite) 2014-009D 39575						Re-entered - 2014 Jul 24 Life 147 days
1U CubeSat to test Lithium-Ion Capacitors for use as a power source in space.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 09:30	6756	0.0010	371	385	92.11	65.00	178

TeikyoSat 3 2014-009E 39576						Re-entered - 2014 Oct 25 Life 240 days
Biological research satellite for Teikyo University, Japan. An onboard camera will observe and transmit images of growth in the slime mould Dictyostelium Discoideum.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 13:12	6767	0.0007	384	394	92.34	65.02	302

INVADER (Interactive satellite for Art and Design Experimental Research) 2014-009F 39577						Re-entered - 2014 Sep 2 Life 187 days
1U Cubesat from Tama Art University, Japan, to be used as a tool in creating art from orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 13:05	6765	0.0007	382	391	92.29	65.01	347

KSat 2 (Kagoshima University Satellite) 2014-009G 39578						Re-entered - 2014 May 18 Life 80 days
1U CubeSat, will study water vapour in the Earth's atmosphere and obtain Earth images. It will also test a pantograph design extending boom and will be used for a number of other space-related experiments.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 13:04	6765	0.0007	382	392	92.29	65.01	348

STARS 2 (Space Tethered Autonomous Robotic Satellite) 2014-009H 39579						Re-entered - 2014 Apr 26 Life 58 days
Space technology payload for Kagawa University, Japan - a pair of satellites joined by a tether to be used in gravity gradient stabilisation experiments, and for experiments in producing an electric current as the tether passes through the Earth's magnetic field.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 13:05	6769	0.0009	384	397	92.36	65.01	287

H-IIA upper stage 2014-009J 39580						Re-entered - 2014 Jun 16 Life 109 days
Launched GPM Core and small satellites, perigee was lowered after satellite release as a collision avoidance manoeuvre and to hasten re-entry.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Feb 28, 11:00	6746	0.0012	359	376	91.89	65.03	357

2014-I14 Nanoracks Cubesat Deployer International Space Station						2014 Feb 28, 04:20
Flock 1A-27 1998-067EJ 39565						Re-entered - 2014 May 3 Life 64 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Time shown is as planned, actual release time to be confirmed. Name/designation are as listed by SpaceTrack. May have been damaged in collision with Flock 1-28, orbit decayed rapidly as a result.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Mar 1, 12:47	6789	0.0011	403	418	92.78	51.66	192

Flock 1A-28 1998-067EK 39566						Re-entered - 2014 Jun 3 Life 95 days
3U Cubesat, part of Planet Labs "Flock 1A" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster. Time shown is as planned, actual release time to be confirmed. Name/designation are as listed by SpaceTrack. May have been damaged in collision with Flock 1-27, orbit decayed quickly as a result.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Mar 1, 12:47	6789	0.0011	403	418	92.79	51.66	192

2014-I15 Nanoracks Cubesat Deployer International Space Station						2014 Feb 28, 06:30
SkyCube 1 1998-067EL 39567						Re-entered - 2014 Nov 8 Life 253 days
1U Cubesat - built using crowdsourcing for funds. Aimed to 'Tweet' from space and provide Earth images on demand from users with a smartphone App. Near the end of life, it was intended to inflate a balloon to make it more visible and to accelerate orbit decay. In the event, the solar panels and aerials did not deploy on reaching orbit and, as a result, the balloon did not inflate. The mission was declared a loss on July 28. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Mar 1, 14:21	6790	0.0007	407	417	92.80	51.65	213

UAPSat 1998-067EM 39568						Re-entered - 2014 May 22 Life 83 days
1U Cubesat from Universidad Alas Peruanas (University of Peru. Carries amateur radio receivers and transmitters and will be controlled by students and staff of the university. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Mar 1, 12:46	6790	0.0005	408	415	92.79	51.64	262

LituanicaSat 1998-067EN 39569						Re-entered - 2014 Jul 28 Life 150 days
1U Cubesat - transmits a message to identify itself and its nationality. Also carries a radio-repeater, an Earth imaging camera and technology test equipment including a range of microcontrollers and attitude sensors. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Mar 1, 12:48	6790	0.0005	408	415	92.80	51.65	230

LitSat 1998-067EP 39570						Re-entered - 2014 May 23 Life 84 days
1U Cubesat from the Lithuanian Space Association. Technology experiments include a computer, Earth imaging cameras and a packet radio repeater. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Mar 1, 12:46	6790	0.0009	406	418	92.81	51.68	178

Ardusat 2 (Arduino Satellite 2) 1998-067EQ 39571						Re-entered - 2014 Jul 1 Life 123 days
2U Cubesat built around an Arduino processor and a set of sensors that can be programmed by students to conduct experiments. Carried to ISS by Cygnus Orb 1 (2014-003A/39502) as part of the Nanoracks CM3 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Mar 1, 14:21	6791	0.0004	410	416	92.82	51.65	225

2014-010 Proton-M + Briz-M Baikonur Cosmodrome						2014 Mar 15, 23:08
Express-AT1 2014-010A 39612						in space
Russian domestic comsat providing fixed and mobile satellite communications, data services, broadband, software distribution and TV to Russia and neighboring countries. Test location 69°.5 east, operational location - 56° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Mar 23, 00:25	42072	0.0040	35523	35864	1431.34	0.16	149	69°.7 E
2014 Mar 31, 15:32	42168	0.0003	35777	35802	1436.25	0.07	93	69°.4 E
2014 Apr 5, 20:22	42275	0.0002	35888	35905	1441.73	0.05	185
2014 Apr 11, 16:21	42207	0.0009	35789	35868	1438.23	0.06	40	55°.7 E
2023 Feb 13, 07:33	42164	0.0000	35786	35786	1436.07	0.04	51	56°.0 E

Express-AT2 2014-010B 39613						in space
Russian domestic comsat providing fixed and mobile satellite communications, data services, broadband, software distribution and TV to Russia and neighboring countries. Operational location (targeted for 2014 late-May) - 140° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Mar 23, 02:02	41970	0.0045	35405	35780	1426.18	0.15	156
2014 Mar 26, 19:56	42086	0.0029	35585	35831	1432.07	0.09	135	77°.6 E
2014 Apr 9, 12:06	42164	0.0001	35779	35792	1436.04	0.05	255	69°.5 E
2014 Apr 19, 13:56	41988	0.0009	35570	35649	1427.07	0.06	54
2014 May 16, 16:00	42064	0.0013	35631	35741	1430.96	0.10	65	135°.9 E
2014 May 24, 19:42	42165	0.0001	35784	35789	1436.10	0.05	218	139°.9 E
2023 Feb 12, 16:22	42165	0.0001	35781	35793	1436.11	0.04	102	139°.8 E

2014-011 Ariane 5ECA (VA-216) Centre Spatiale Guyanaise						2014 Mar 22, 22:04
Amazonas 4A 2014-011A 39616						in space
Communications services for South America. Expected location - 61° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Mar 25, 04:00	26451	0.5894	4481	35664	713.53	1.87	179
2014 Mar 27, 14:47	31897	0.3181	15373	35665	944.92	0.78	181
2014 Mar 31, 11:42	42083	0.0002	35699	35712	1431.94	0.04	3	53°.1 W
2014 Apr 5, 05:32	42164	0.0001	35780	35792	1436.08	0.04	4	51°.0 W
2014 Sep 14, 03:58	42243	0.0002	35855	35874	1440.08	0.09	281
2014 Sep 25, 11:06	42165	0.0003	35775	35800	1436.13	0.03	114	61°.0 W
2023 Feb 13, 11:01	42164	0.0003	35771	35800	1436.05	0.02	237	74°.0 W

Astra 5B 2014-011B 39617						in space
Comsat to cover Eastern Europe with Direct to Home and cable feeds to digital television networks. It also carries a hosted L-band payload for the European Commission’s European Geostationary Navigation Overlay Service (EGNOS). Expected location 31°.5 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Mar 23, 12:04	24367	0.7277	257	35721	630.91	3.02	178
2014 Mar 26, 03:20	29733	0.4156	10999	35711	850.38	1.10	178
2014 Mar 27, 01:42	37962	0.1089	27450	35717	1226.81	0.29	177
2014 Apr 5, 01:38	42164	0.0000	35785	35787	1436.06	0.13	288	43°.5 E
2014 May 15, 02:14	42215	0.0000	35836	35837	1438.64	0.07	137	42°.0 E
2014 Jun 3, 15:50	42165	0.0002	35779	35794	1436.09	0.08	60	31°.6 E
2023 Feb 13, 02:55	42165	0.0003	35773	35800	1436.09	0.05	16	31°.5 E

2014-012 Soyuz-2.1b + Fregat Plesetsk Cosmodrome						2014 Mar 23, 22:54
Cosmos 2492 (Uragan-M № 748) 2014-012A 39620						in space
GLONASS-M navigation satellite. Separated from the launch vehicle Mar 24 at 02:26 UTC. NOTE - the Cosmos number is out of sequence.. An error by the Russian Ministry of Defence led to it being called Cosmos 2491 in press releases and on the official GLONASS status website. It was previously listed here as Cosmos 2494.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Mar 24, 15:26	25519	0.0005	19128	19153	676.17	64.81	274
2014 Apr 21, 22:52	25508	0.0018	19083	19176	675.73	64.82	329

2014-013 Soyuz-FG 11A511U-FG Baikonur Cosmodrome						2014 Mar 25, 21:17
Soyuz TMA-12M (Soyuz 11F732A47 № 712) 2014-013A 39622						Re-entered - 2014 Sep 11 Life 170 days Returned to Earth
Crew to ISS - Alexander Skvortsov, Oleg Artemyev and Steve Swanson. Precise launch time - 23:33:53 UTC. Intended to follow the 6hr 'fast track' trajectory to the ISS but changed to a two-day approach after a problem with the Soyuz orientation system occurred around three hours into the mission. Docked with the port on Poisk Mar 27 at 23:33:53 UTC. Undocked September 10 at 23:02 UTC carrying Skortsov, Artemyev and Swanson. Retro-fire September 11 at 01:31 UTC led to a landing 148 km south-east of Dzhezkazgan, Kazakhstan at 02:23 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Mar 25, 21:06	6597	0.0038	194	244	88.88	51.65	90
2014 Mar 26, 01:58	6694	0.0029	297	335	90.85	51.65	113
2014 Mar 26, 07:53	6822	0.0065	400	488	93.46	51.64	345
2014 Mar 26, 12:48	6798	0.0008	414	425	92.97	51.65	22
2014 Mar 27, 08:58	6801	0.0004	420	426	93.04	51.64	351
2014 Mar 27, 18:15	6792	0.0004	411	416	92.84	51.65	1

2014-014 CZ 2C Jiuquan Space Centre						2014 Mar 31, 02:46
Shijian 11-06 (Practice 11-06) 2014-014A 39624						in space
Reported as an "experimental satellite". The orbit, and images of one of its predecessors, indicate that it has an Earth observation rôle. Launch time is an estimate based on the local time at the Descending Node and is ±1 minute. China announced a time of 02:58 UTC but it probably represents when the satellite separated from the launch vehicle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Apr 1, 02:53	7074	0.0012	688	704	98.69	98.26	212	09:02
2023 Feb 13, 10:09	7073	0.0014	685	705	98.67	98.10	209	08:40

2014-015 Atlas V 401, AV-044 Vandenberg Air Force Base						2014 Apr 3, 14:46
USA 249 (DMSP 5D-3 F-19) 2014-015A 39630						in space
Vehicle in the US Defense Meteorological Satellite Program for collecting strategic weather and climate data. Precise launch time 14:46:30 UTC, separated from the launch vehicle at 15:04 UTC. Centaur stage of Atlas launch vehicle was 'disposed of' by sending it to Heliocentric orbit.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Apr 8, 14:47	7225	0.0010	839	853	101.85	98.85	282	06:29
2023 Feb 13, 12:36	7223	0.0012	837	854	101.83	98.75	87	05:50

2014-016 Soyuz ST-A + Fregat-M (VS-07) Centre Spatiale Guyanaise						2014 Apr 3, 21:02
Sentinel 1A 2014-016A 39634						in space
First of a pair of satellites equipped with an imaging Synthetic Aperture Radar (SAR) to provide an all-weather day-and-night supply of imagery. The satellite is part of ESA's Copernicus constellation, the EU contribution to GEOSS (Global Earth Observation System of Systems). Precise launch time: 21:02:26 UTC, separated from the launch vehicle at 21:25:50 UTC. The Fregat stage of the Soyuz re-entered above the southern Atlantic Ocean around 22:45 UTC and was not catalogued.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Apr 4, 05:20	7066	0.0003	686	690	98.52	98.17	67	06:00
2014 May 26, 19:15	7068	0.0002	688	691	98.55	98.16	94	06:00
2014 Jul 31, 02:22	7073	0.0002	694	696	98.67	98.18	88	06:00
2023 Feb 13, 09:55	7074	0.0001	695	697	98.68	98.18	84	06:01

2014-017 PSLV-XL (PSLV C-24) Satish Dhawan Space Centre						2014 Apr 4, 11:44
IRNSS 1B (Indian Regional Navigation Satellite System 1B) 2014-017A 39635						in space
Satellite in the Indian Regional Navigation Satellite System aimed at inclined geosynchronous orbit, separated from the launch vehicle at 12:03 UTC. Expected location 55° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Apr 4, 15:03	16792	0.6041	270	20558	360.93	19.26	178
2014 Apr 7, 15:44	30222	0.4000	11754	35934	871.45	26.93	179
2014 Apr 10, 14:31	42051	0.0061	35417	35930	1430.31	30.99	179	44°.8 E
2014 Apr 15, 18:56	42100	0.0037	35566	35878	1432.79	30.99	180	49°.6 E
2014 Apr 24, 13:54	42166	0.0022	35695	35880	1436.14	30.97	182	55°.0 E

2014-018 Soyuz-U 11A511U Baikonur Cosmodrome						2014 Apr 9, 15:26
Progress M-23M (Progress 7K-TGM №427) 2014-018A 39648						Re-entered - 2014 Jul 31 Life 113 days
Supplies to ISS. Precise launch time 15:26:27 UTC. Docked with the Pirs module at 21:14 UTC, six minutes earlier than anticipated. Undocking 2014 July 24 at 21:44 UTC was followed by a period of Radar-Progress experiments. Retrofire July 31 at 21:51 UTC led to destructive re-entry above the southern Pacific Ocean at 22:30 UTC, any surviving fragments hit the water near 51° south, 131° west about 13 minutes later.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Apr 9, 15:15	6580	0.0024	186	218	88.54	51.64	59
2014 Apr 9, 20:10	6772	0.0029	374	414	92.44	51.64	66
2014 Apr 10, 11:38	6793	0.0002	413	416	92.86	51.65	12

2014-019 Shavit 2? Palmachim AFB, Israel						2014 Apr 9, 19:06
Ofeq 10 (Horizon 10) 2014-019A 39650						Re-entered - 2024 Jul 14 Life 3749 days
Israeli reconnaissance satellite monitoring the Middle East from highly retrograde orbit. Equipped with an imaging radar. The first two listed orbits are estimates based on limited data provided by SpaceTrack, all others are based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Apr 9, 20:30	6849	0.0202	332	609	94.01	140.94	90
2014 Apr 12, 19:00	6877	0.0157	391	607	94.60	140.94	90
2014 Apr 30, 02:28	6871	0.0157	385	601	94.47	140.94	231
2015 Nov 2, 16:38	6859	0.0031	459	502	94.22	141.00	340

2014-020 Atlas V 541, AV-045 Cape Canaveral Air Force Station						2014 Apr 10, 17:45
USA 250 (SIGINT?) 2014-020A 39652						in space
Probably a Signals Intelligence gathering (SIGINT) satellite. Orbits based on amateur observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2016 Oct 25, 05:43	42165	0.0003	35773	35801	1436.12	3.06	276	163°.0 W
2017 Mar 21, 03:41	42355	0.0007	35947	36007	1445.81	2.82	77
2017 Apr 17, 02:01	42165	0.0004	35770	35804	1436.12	2.80	42	82°.0 E
2020 Sep 14, 19:29	42165	0.0004	35770	35804	1436.12	1.41	10	82°.1 E

Atlas upper stage (Centaur) 2014-020B 39653						in space
Launched USA 250.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2015 Jan 27, 17:44	27927	0.4868	7955	35142	774.09	11.28	232

2014-021 Soyuz-U 11A511U Baikonur Cosmodrome						2014 Apr 16, 16:20
Egyptsat 2 2014-021A 39678						in space
Egyptian remote sensing satellite built under contract by Russia's Energiya company. Separated from launch vehicle at 16:28 UTC. Launch was put on hold 2011 following all contact being lost with EgyptSat 1. Orbit requirement was subsequently changed from sun-synchronous. From April 30 to July 11, Egyptsat 2 fired a thruster at successive passages through orbital apogee in order to produce the 714 km, circular, operational orbit. A major system failure around 2015 Apr 12 means that the satellite is no longer operating.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Apr 17, 04:55	6948	0.0192	436	703	96.05	51.61	82
2014 Apr 29, 04:53	6947	0.0193	435	703	96.05	51.61	123
2014 May 5, 11:18	6949	0.0189	440	703	96.09	51.62	144
2014 May 6, 11:18	6950	0.0187	442	703	96.11	51.62	148
2014 May 13, 18:00	6963	0.0172	465	704	96.37	51.62	173
2014 May 20, 22:04	6980	0.0144	501	702	96.72	51.62	198
2014 May 27, 10:35	6993	0.0127	526	704	97.00	51.62	219
2014 Jun 3, 17:19	7006	0.0108	552	704	97.27	51.61	245
2014 Jun 10, 03:29	7021	0.0089	580	706	97.58	51.61	269
2014 Jun 16, 12:36	7041	0.0065	617	708	97.99	51.62	288
2014 Jun 23, 11:30	7064	0.0036	660	711	98.47	51.62	313
2014 Jun 30, 09:28	7079	0.0017	689	713	98.80	51.62	338
2014 Jul 11, 04:16	7092	0.0003	711	716	99.06	51.62	127
2014 Jul 18, 04:34	7092	0.0001	713	714	99.06	51.62	96

2014-022 Falcon 9 v1.1 Cape Canaveral Air Force Station						2014 Apr 18, 19:25
SpaceX Dragon CRS-3 2014-022A 39680						Re-entered - 2014 May 18 Life 30 days Returned to Earth
Carrying a cargo to the ISS under NASA's Commercial Resupply Services (CRS) contract. Precise launch time 19:25:22 UTC. Captured by ISS Remote Manipulator at exactly the planned time - Apr 20, 11:14 UTC. Attached to the downward-facing port of Harmony at 14:00 UTC, 15 minutes later than planned. Securing bolts were driven home six minutes later. Undocked using the SSRMS May 18 at 12:00 UTC. Retrofire the same day at 18:12 UTC led to spashdown in the Pacific Ocean at 19:05 near 29°.5 north, 121°.2 west. The launching rocket was not catalogued because it was caused to re-enter above the Indian Ocean about 2.5 hrs after launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Apr 18, 19:40	6701	0.0014	313	332	90.98	51.64	268
2014 Apr 19, 04:27	6703	0.0012	317	333	91.04	51.65	247
2014 Apr 19, 09:00	6699	0.0018	309	333	90.95	51.65	275
2014 Apr 20, 07:04	6784	0.0003	404	408	92.68	51.65	1
2014 Apr 20, 08:26	6795	0.0003	414	419	92.90	51.65	307

SporeSat 2014-022B 39681						Re-entered - 2014 Jun 4 Life 47 days
3U Cubesat to study how plant cells sense gravity, joint mission between NASA’s Ames Research Center and the Department of Agricultural and Biological Engineering at Purdue University. Part of NASA ELaNa 5 Cubesat initiative.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Apr 19, 15:02	6694	0.0022	301	331	90.85	51.64	273

TSat (TESTSat-Lite) 2014-022C 39682						Re-entered - 2014 May 28 Life 40 days
2U Cubesat from Taylor University, Indiana, will use a GlobalStar satellite communication modem to demonstrate a reliable and global nanosat network, and will observe space weather with a plasma probe, 3-axis magnetometer, and three ultraviolet photodiodes. Part of NASA ELaNa 5 Cubesat initiative.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Apr 19, 05:57	6695	0.0023	301	332	90.85	51.65	268

ALLSTAR/THEIA 2014-022D 39683						Re-entered - 2014 May 26 Life 38 days
3U Cubesat, sponsored by the Colorado Space Grant Consortium (CoSGC) and Lockheed Martin, for full-colour imaging of the Earth's surface to demonstrate the capabilities of a new Cubesat design. Part of NASA ELaNa 5 Cubesat initiative. NOTE - prior to 2014 May, ALLSTAR/THEIA was catalogued as 2014-022E/39684.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Apr 19, 05:57	6695	0.0023	301	332	90.86	51.67	274

Phonesat 2.5 2014-022E 39684						Re-entered - 2014 May 15 Life 27 days
1U Cubesat from NASA Ames laboratory, fourth in a series of missions designed to use commercially available smartphone technology as part of low-cost satellite development, technology demonstrator as a pathfinder for the Edison Demonstration of Smallsat Network. Part of NASA ELaNa 5 Cubesat initiative. NOTE - prior to 2014 May, Phonesat 2.5 was catalogued as 2014-022D/39683.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Apr 19, 21:05	6695	0.0019	304	330	90.86	51.65	274

KickSat 2014-022F 39685						Re-entered - 2014 May 14 Life 26 days
3U Cubesat holding 104 postage stamp shape/size (35mm x 35mm) individual satellites for organisations that sponsored them - each satellite was designed to transmit a unique code to identify mission sponsors plus data from a small sensor. They were intended to be released May 4 at 19:40 UTC as a result of a timer set for 16 days after Kicksat activation. On Apr 30, an unexpected hardware 'reset' caused the timer to re-start and set release for May 16 - Kicksat, unfortunately, re-entered on May 14. KickSat itself carried carries logos and signatures of individuals and organisations that sponsored the launch with donations. Part of NASA's ELaNa 5 Cubesat initiative.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Apr 19, 08:59	6694	0.0024	299	331	90.83	51.65	273

2014-023 Proton-M + Briz-M Baikonur Cosmodrome						2014 Apr 28, 04:25
Luch 5V 2014-023A 39727						in space
Designed to relay commands and data to and from satellites in LEO up to 2000 kilometres when outside the the areas covered by Russian ground stations. Other functions include secure Presidential communication links, command relay to rockets and spacecraft, and communication with the International Space Station. It will also provide time correction for GLONASS users. Separated from the Briz-M at 13:17 UTC in near-geosynchronous orbit. Expected location - 95° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 May 1, 18:33	41956	0.0046	35387	35769	1425.45	4.84	350
2014 May 13, 12:13	42094	0.0004	35697	35734	1432.47	4.77	332	92°.0 E
2014 May 22, 11:48	42163	0.0004	35769	35800	1436.00	4.75	123	94°.9 E
2023 Feb 13, 01:30	42166	0.0003	35775	35801	1436.16	2.08	271	94°.7 E

Kazsat 3 2014-023B 39728						in space
Communications satellite for Kazakhstan to provide point-to-point links, TV and high-speed Internet. Separated from the Briz-M at 13:57 UTC into geosynchronous drift orbit. Expected location - 58°.5 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 May 8, 19:51	42156	0.0033	35639	35916	1435.63	0.22	243	81°.1 E
2014 May 10, 20:21	42268	0.0025	35787	35994	1441.40	0.22	267
2014 May 27, 15:06	42164	0.0001	35784	35789	1436.08	0.12	155	58°.5 E
2023 Feb 13, 09:55	42164	0.0001	35783	35789	1436.08	0.01	203	58°.5 E

2014-024 Vega (VV-03) Centre Spatiale Guyanaise						2014 Apr 30, 01:35
KazEOSat 1 (DZZ-HR) 2014-024A 39731						in space
High-resolution observation satellite owned by Kazakhstan, tasks including monitoring of natural and agricultural resources, provision of mapping data, and support for rescue operations in the event of a natural disaster. KazEOSat stands for "Kazcosmos Earth Observation Satellite". Precise launch time 01:35:15 UTC. Separated from the launch vehicle at 02:30:44 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 May 1, 02:29	7118	0.0001	739	741	99.60	98.56	104	10:14
2023 Feb 13, 09:42	7130	0.0001	751	753	99.86	98.44	78	10:37

2014-025 Soyuz-2.1a Plesetsk Cosmodrome						2014 May 6, 13:49
Cosmos 2495 (Yantar 4K2M 11Ф695M, Kobalt-M) 2014-025A 39732						Re-entered - 2014 Sep 2 Life 119 days Returned to Earth
Military imaging reconnaissance satellite, sometimes referred to as 'Yantar', with manoeuvring engine to maintain its orbit. Dropped off two containers of exposed film at different times during the mission for retro-fire and recovery - the first one landed, probably near Orenburg, June 6 at about 08:08 UTC and the second one in, the same area, July 3 at around 04:01 UTC. The main camera/film module was recovered near Orenburg on Sep 2 at 18:27 UTC following retro-fire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 May 6, 21:16	6609	0.0083	176	285	89.12	81.41	88
2014 May 13, 21:15	6602	0.0047	193	256	88.98	81.41	72

2014-F01 - failed to reach orbit Proton-M + Briz-M Baikonur Cosmodrome						2014 May 15, 21:42
Express-AM4R
Russian domestic communications satellite, replacement for Express AM-4. Destroyed at L+545s, approaching the end of third stage engine firing, when the turbopump bearing of the steering engine disintegrated. Debris fell on China.

2014-026 Delta 4 Medium+ 4,2 Cape Canaveral Air Force Station						2014 May 17, 00:03
USA 251 (Navstar GPS IIF-06) 2014-026A 39741						in space
Sixth Block 2F, Generation 2 GPS Navsat. Launched at the the opening of an 18 minute window. May 16 launch attempt postponed about 1 hr before planned lift-off because of weather.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 May 17, 05:03	26837	0.0006	20444	20474	729.22	55.04	138

2014-027 Atlas V 401, AV-046 Cape Canaveral Air Force Station						2014 May 22, 13:09
USA 252 (SDS [-3 F-7?] ) 2014-027A 39751						in space
Probably a third generation Satellite Data System government/military communications satellite aimed at geosynchronous orbit. Launch delayed 4 min from originally announced time, reportedly to avoid a possible collision with an object already in orbit. The Centaur stage of the Atlas V was not catalogued - it was intentionally sent toward a destructive re-entry at the end of its first circuit. Any surviving fragments hit the Surface of the Pacific Ocean shortly after 22:00 UTC near 14° north, 175° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
estimated orbit	21417	0.6897	268	29809	519.86	21.20	183
2015 Mar 15, 15:06	42165	0.0004	35769	35805	1436.12	4.33	213	144°.0 W
2016 Jul 22, 12:56	42166	0.0003	35776	35800	1436.16	3.40	225	170°.0 E

2014-028 Rockot + Briz-KM Plesetsk Cosmodrome						2014 May 23, 05:27
Cosmos 2496 (Strela-3M/Rodnik) 2014-028A 39761						in space
Government/military system store-dump communications satellite. Precise launch time: 05:27:54 UTC, released from the Briz-KM at 07:12.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 May 24, 13:49	7873	0.0020	1480	1511	115.88	82.44	318

Cosmos 2497 (Strela-3M/Rodnik) 2014-028B 39762						in space
Government/military system store-dump communications satellite. Precise launch time: 05:27:54 UTC, released from the Briz-KM at 07:12.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 May 23, 22:22	7872	0.0020	1478	1510	115.85	82.45	316

Cosmos 2498 (Strela-3M/Rodnik) 2014-028C 39763						in space
Government/military system store-dump communications satellite. Precise launch time: 05:27:54 UTC, released from the Briz-KM at 07:12.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 May 24, 13:48	7871	0.0020	1477	1509	115.82	82.44	310

Cosmos 2499 (RS-47) 2014-028E 39765						in space
Small satellite with low thrust ion engine to demonstrate orbit changing capability. Used its own Briz-KM rocket body (2014-028D/39764) as a station-keeping target. Detected by US tracking sensors and originally catalogued as debris, it was not included in early announcements of the launch. Early 2014 July - started a series of manoeuvres to reduce the separation in orbit planes between itself and the Briz-KM. 2014 November 8/9 it matched planes with the rocket and manoeuvred alongside it, co-orbiting within a few tens of metres. The experiment may then have been complete because, as of 2014 Dec 1, the satellite began identifying itself as amateur radio satellite Radio Sputnik 47 (RS-47). 2021 Dec - Space-Track reported 22 debris items from a partial break-up that occurred on Oct 23 that year at ~20:00 UTC. Further disintegrated 2023 Jan 4.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 May 23, 20:26	7872	0.0018	1480	1509	115.86	82.45	317
2014 May 29, 21:19	7873	0.0018	1481	1508	115.86	82.45	304
2014 Jul 2, 22:32	7872	0.0017	1480	1508	115.85	82.45	228
2014 Jul 3, 19:47	7871	0.0020	1477	1508	115.82	82.45	218
2014 Jul 9, 09:02	7868	0.0024	1472	1509	115.77	82.46	200
2014 Jul 11, 17:00	7866	0.0021	1471	1504	115.71	82.45	189
2014 Jul 17, 15:46	7855	0.0022	1460	1494	115.47	82.46	166
2014 Aug 8, 16:11	7684	0.0241	1121	1491	111.72	82.46	99
2014 Aug 12, 10:19	7621	0.0323	997	1489	110.36	82.46	94
2014 Aug 20, 09:32	7588	0.0337	954	1465	109.63	82.42	78
2014 Aug 20, 14:25	7585	0.0371	925	1488	109.57	82.45	73
2014 Oct 28, 23:22	7652	0.0287	1055	1494	111.03	82.46	254
2014 Nov 9, 00:02	7681	0.0254	1108	1499	111.67	82.45	231
2014 Nov 9, 13:19	7705	0.0228	1152	1503	112.19	82.46	230
2014 Dec 12, 02:52	7706	0.0230	1151	1505	112.20	82.44	156
2023 Feb 3, 22:25	7708	0.0232	1151	1509	112.25	82.45	8

Briz-KM 2014-028D 39764						in space
Launched Strela/Rodnik Cluster and Cosmos 2499.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 May 25, 13:10	7706	0.0229	1151	1504	112.19	82.44	268
2014 Nov 8, 03:10	7706	0.0228	1152	1503	112.19	82.44	236

2014-029 H-IIA 202 (F-24) Tanegashima Space Centre						2014 May 24, 03:05
Daichi 2 (ALOS 2, Advanced Land Observation Satellite 2) 2014-029A 39766						in space
Advanced Land Observing Satellite for remote sensing using radar. Precise launch time 03:05:14 UTC at the opening of a launch window that closed at 03:19:07. Separated from the launch vehicle at 03:21:01 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 May 24, 12:18	7011	0.0004	630	635	97.36	97.88	189	12:00
2023 Feb 13, 10:45	7009	0.0002	630	632	97.33	97.92	93	11:59

UNIFORM 1 (UNiversity International FORmation Mission 1) 2014-029B 39767						in space
Small satellite resulting from co-operation between several Japanese universities led by Wakayama University. It carries a payload designed to demonstrate how a constellation of satellites can be used to monitor wildfires on the Earth.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 May 25, 01:15	7004	0.0005	622	629	97.22	97.87	11	12:00
2023 Feb 13, 05:55	6990	0.0006	608	617	96.94	97.83	32	11:40

SOCRATES (Space Optical Communications Research Advanced TEchnology Satellite) 2014-029C 39768						in space
Demonstrator vehicle for a satellite bus from the Japanese company AES (Advanced　Engineering　Services) Co Ltd.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 May 25, 09:21	7001	0.0008	618	629	97.17	97.87	37	12:00
2023 Feb 13, 10:11	6989	0.0007	606	616	96.92	97.87	52	12:07

Rising 2 2014-029D 39769						in space
Small satellite for remote sensing from Tohoku University, Japan. The optical system is equipped with a liquid crystal tunable filter to allow multispectral observations including stereo imaging of cumulo-nimbus clouds and detection of luminous events in the upper atmosphere.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 May 25, 04:31	7006	0.0003	625	630	97.27	97.88	340	12:00
2023 Feb 13, 10:52	6998	0.0005	616	623	97.10	97.78	30	10:54

SPROUT (SPace Research On Unique Technology) 2014-029E 39770						Re-entered - 2024 Aug 11 Life 3732 days
Carries amateur radio relay equipment and will demonstrate deployment of a sheet of flexible material held between inflatable 'poles' , built by students from Nihon University, Japan.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 May 25, 02:53	6999	0.0011	614	629	97.13	97.87	50	12:00
2023 Feb 13, 13:34	6958	0.0007	575	584	96.26	97.95	357	13:42

2014-030 Zenit 3SL Sea Launch Platform 'Odyssey', Kiritmati						2014 May 26, 21:09
Eutelsat 3B 2014-030A 39773						in space
Commercial comsat to cover Europe, North Africa, the Middle East and West Asia. Precise time of lift-off - 21:09:59, separated from the launch vehicle at 22:10:28 UTC. Expected location - 3° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 May 28, 09:04	26978	0.5567	5580	35620	734.98	0.03	172
2014 May 29, 15:52	32179	0.3051	15982	35620	957.45	0.08	161
2014 Jun 2, 06:28	36437	0.1527	24495	35623	1153.66	0.04	109
2014 Jun 5, 13:35	42017	0.0003	35625	35653	1428.57	0.04	213	0°.6 E
2014 Jun 6, 14:24	42128	0.0012	35700	35800	1434.24	0.04	236	1°.6 E
2014 Jun 11, 01:37	42165	0.0005	35764	35810	1436.10	0.06	56	1°.6 E
2014 Jul 3, 05:12	42165	0.0002	35777	35796	1436.09	0.07	285	3°.1 E
2023 Feb 12, 09:29	42164	0.0003	35771	35800	1436.05	0.06	237	3°.1 E

2014-031 Soyuz-FG 11A511U-FG Baikonur Cosmodrome						2014 May 28, 19:57
Soyuz TMA-13M (Soyuz 11F732A47 № 713) 2014-031A 39775						Re-entered - 2014 Nov 10 Life 166 days Returned to Earth
Crew to ISS - Reid Wiseman, Maxim Suraev and Alexander Gerst. Precise launch time - 19:57:41 UTC. Docked with ISS Rassvet port May 29 at 01:44:02 UTC, about four minutes ahead of schedule. Undocked Nov 10 at 00:31:30 UTC. Following retro-fire for 281s (Δv 127 m/s) starting at 03:05 UTC, Soyuz-TMA-13M landed 85 km North of Arkalyk, Kazakhstan at 03:58 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 May 28, 20:26	6590	0.0022	198	227	88.74	51.63	74

2014-032 Soyuz-2.1b + Fregat Plesetsk Cosmodrome						2014 Jun 14, 17:16
Cosmos 2500 (Uragan-M № 755) 2014-032A 40001						in space
GLONASS-M navigation satellite to fill a space in the constellation. Released from the Fregat stage at 20:48 UTC and responded to ground control, as expected, at 20:53 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 16, 11:15	25519	0.0005	19129	19153	676.18	64.77	300
2014 Jun 20, 03:21	25582	0.0023	19145	19263	678.67	64.77	47
2014 Jun 29, 03:14	25508	0.0006	19114	19146	675.73	64.77	211

2014-033 Dnepr Dombarovsky (Yasny) Cosmodrome						2014 Jun 19, 19:11
KazEOSat 2 (Kazcosmos Earth Observation Satellite) 2014-033A 40010						in space
Medium-resolution observation satellite owned by Kazakhstan. Known as DZZ-MR before launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 21, 04:41	7002	0.0017	612	636	97.19	97.99	225	22:30
2023 Feb 13, 11:12	7001	0.0014	613	633	97.16	97.69	16	21:30

Hodoyoshi 4 2014-033B 40011						in space
Small, three axis stabilised satellite for Earth imaging from the University of Tokyo, also carries a store and forward comms payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 21, 04:44	7010	0.0027	613	650	97.35	97.99	209	22:30
2023 Feb 13, 10:37	7001	0.0027	604	641	97.15	97.64	12	20:36

Unisat 6 2014-033C 40012						in space
Small satellite with an amateur radio communications system but its principal task is as a Cubesat dispenser for four satellites carried in 3 x 3U launch dispensers. The Cubesats (ANTELSat, Lemur 1, TIgrisat and Aerocube 6) were released June 20 at 21:07 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 21, 01:39	7034	0.0062	613	699	97.86	97.98	196

Deimos 2 2014-033D 40013						in space
Spanish satellite for optical Earth imaging - member of the Disaster Monitoring Constellation, follow-on to Deimos 1 (2009-041A/35681).
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 21, 04:34	6986	0.0016	597	619	96.85	97.99	313	22:30
2023 Feb 13, 10:13	6988	0.0002	609	612	96.90	97.74	73	22:27

BugSat 1 (Tita) 2014-033E 40014						in space
Technology demonstration mission for a new design earth observation satellite, testing aerials, camera, GPS receiver and a radio system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 21, 04:28	6972	0.0034	570	617	96.55	97.99	342	22:30
2023 Feb 13, 06:12	6951	0.0029	553	593	96.12	98.14	324	06:18

Hodoyoshi 3 2014-033F 40015						in space
Small, three axis stabilised satellite for Earth imaging from the University of Tokyo, also carries a store and forward comms payload.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 21, 04:48	7018	0.0038	613	666	97.51	97.98	202	22:30
2023 Feb 12, 20:06	7010	0.0038	605	658	97.34	97.62	40	19:11

SaudiSat 4 2014-033G 40016						in space
Satellite from King Abdulaziz City for Science and Technology (KACST) in Saudi Arabia carrying an experiment jointlydesigned with NASA Ames Reearch Centre to investigate electrostatic build-up.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 21, 04:51	7026	0.0049	613	682	97.68	97.98	198	22:30
2023 Feb 13, 11:43	7020	0.0049	608	677	97.57	97.64	80	17:51

Aurora (Tabletsat-2U-EO) 2014-033H 40017						in space
Russian technology demonstration satellite with an Earth observation still and video camera system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 21, 04:31	6979	0.0025	583	618	96.70	97.99	333	22:30
2023 Feb 13, 09:47	6955	0.0021	563	592	96.22	98.14	342	05:08

Aprizesat 9 2014-033J 40018						in space
Small satellite for data collection from small fixed and mobile ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 21, 04:58	7042	0.0072	613	715	98.03	97.98	193
2023 Feb 13, 10:31	7037	0.0071	609	709	97.92	97.73	159

Aprizesat 10 2014-033K 40019						in space
Small satellite for data collection from small fixed and mobile ground stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 21, 05:02	7052	0.0085	613	733	98.22	97.98	192
2023 Feb 13, 09:38	7047	0.0083	610	727	98.12	97.79	207

BRITE-Toronto (BRIght Target Explorer) 2014-033L 40020						in space
One of six satellites in a Canadian constellation to make astronomical observations, particularly long-duration observations of bright stars with extremely long periods of oscillation. Expected orbit - approx 613 x 763 km.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 22, 12:12	7054	0.0089	613	739	98.27	97.97	187	22:29
2023 Feb 13, 08:36	7047	0.0085	609	729	98.13	97.80	215	15:33

DUCHIFAT 2014-033M 40021						in space
1U Cubesat buily by secondary school students at the Space Laboratory of the Herzliya Science Centre, Israel with support from the Israeli Amateur Radio Organization, it will transmit real-time information using the Automatic Position Reporting System (APRS) protocol. Initial identification by Nico Janssen using radio Doppler measurement.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 10:13	6991	0.0012	604	621	96.95	97.98	276
2023 Feb 13, 03:35	6959	0.0011	574	589	96.30	98.04	335

Flock 1C-10 2014-033N 40022						in space
3U Cubesat, part of Planet Labs "Flock 1C" consisting of 11 Earth imaging satellites. Catalogue number, ID and precise orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 20:19	6991	0.0013	604	622	96.95	97.99	274
2023 Feb 13, 01:38	6972	0.0013	585	603	96.56	97.98	360

PACE (Platform for Attitude Control Experiments) 2014-033P 40023						in space
2U Cubesat developed by students at the National Cheng Kung University (NCKU) in Tainan, Taiwan to verify and evaluate varying attitude determination and control strategies. Catalogue number, ID and precise orbit to be confirmed.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 16:41	6991	0.0012	604	621	96.95	97.99	275
2023 Feb 13, 02:30	6961	0.0011	576	591	96.34	98.03	354

NanosatC-Br1 2014-033Q 40024						in space
1U Cubesat from Brazil's Southern Regional Space Research Cente, built in collaboration with the Space Science Laboratory of the Federal University of Santa Maria and the Brazilian Space Agency - INPE. Initial association with ID and catalogue number by Nico Janssen using radio Doppler measurement.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 03:45	6991	0.0011	605	621	96.96	97.98	279
2023 Feb 13, 02:19	6964	0.0011	579	593	96.40	98.01	345

QB50p1 2014-033R 40025						in space
2U Cubesat, one of a pair of precursor satellites for the QB50 project. Carries an Ion and Neutral Mass Spectrometer to study the Earth's lower thermosphere. Initial association with ID and catalogue number by Nico Janssen using radio Doppler measurement.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 10:13	6991	0.0011	605	621	96.96	97.98	278
2023 Feb 13, 13:31	6969	0.0011	583	599	96.50	97.98	352

Flock 1C-7 2014-033S 40026						Re-entered - 2025 Feb 8 Life 3887 days
3U Cubesat, part of Planet Labs "Flock 1C" consisting of 11 Earth imaging satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 10:13	6991	0.0011	606	620	96.96	97.99	277
2023 Feb 13, 02:45	6953	0.0008	569	580	96.16	98.05	348

Flock 1C-1 2014-033T 40027						in space
3U Cubesat, part of Planet Labs "Flock 1C" consisting of 11 Earth imaging satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 23, 13:12	6991	0.0012	605	621	96.96	97.99	279

POPSAT-HIP 2014-033U 40028						in space
3U Cubesat from Microspace Rapid of Singapore equipped with an imaging system and a cold gas thruster system for attitude control. Initial association with ID and catalogue number by Nico Janssen using radio Doppler measurement.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 10:14	6992	0.0013	604	623	96.97	97.99	272
2023 Feb 13, 09:16	6970	0.0013	583	601	96.53	98.00	354

Flock 1C-2 2014-033V 40029						in space
3U Cubesat, part of Planet Labs "Flock 1C" consisting of 11 Earth imaging satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 10:15	6992	0.0013	605	623	96.98	97.99	270
2023 Feb 13, 07:17	6957	0.0011	571	586	96.24	98.03	346

DTUSat 2 2014-033W 40030						in space
1U Cubesat from the National Space Institute at the Technical University of Denmark to provide a spaceborne radio-tracking system capable of locating birds fitted with transmitters on their migration routes.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 25, 04:02	6992	0.0012	606	622	96.98	97.98	264

Flock 1C-4 2014-033X 40031						in space
3U Cubesat, part of Planet Labs "Flock 1C" consisting of 11 Earth imaging satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 03:47	6992	0.0012	606	622	96.98	97.99	271

QB50p2 2014-033Y 40032						in space
2U Cubesat, one of a pair of precursor satellites for the QB50 project. Carries FIPEX (Φ Probe Experiment) to study the presence of atomic Oxygen. Initial association with ID and catalogue number by Nico Janssen using radio Doppler measurement.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 10:15	6992	0.0011	607	622	96.98	97.98	268
2023 Feb 12, 21:13	6971	0.0011	586	601	96.55	97.96	353

Flock 1C-11 2014-033Z 40033						in space
3U Cubesat, part of Planet Labs "Flock 1C" consisting of 11 Earth imaging satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 10:15	6992	0.0012	606	622	96.98	97.99	265
2023 Feb 13, 04:55	6953	0.0009	569	581	96.17	98.06	328

ANTELSat 2014-033AA 40034						in space
2U Cubesat from Uruguay's Universidad de la República and the government owned ANTEL (Administración Nacional de Telecomunicaciones). It carries developmental communications systems operating at VHF,UHF and S-band, and an Earth-imaging system with detectors in the near infrared and visible bands. Released from Unisat 6 June 20 at 21:07:00 from the same deployer as Aerocube 6.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 10:15	6992	0.0012	606	623	96.99	97.99	267
2023 Feb 13, 05:38	7019	0.0058	601	682	97.54	97.66	96

Flock 1C-9 2014-033AB 40035						Re-entered - 2025 Feb 4 Life 3883 days
3U Cubesat, part of Planet Labs "Flock 1C" consisting of 11 Earth imaging satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 10:16	6993	0.0012	607	623	96.99	97.99	261
2023 Feb 13, 07:15	6956	0.0009	572	584	96.24	98.04	341

Flock 1C-6 2014-033AC 40036						in space
3U Cubesat, part of Planet Labs "Flock 1C" consisting of 11 Earth imaging satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 10:16	6993	0.0011	607	622	96.99	97.99	263
2023 Feb 13, 03:38	6955	0.0009	570	583	96.20	98.04	338

Perseus-M 2 2014-033AD 40037						in space
6U Cubesat (3x2) from Dauria Aerospace equipped with a remote sensing imaging system and a receiver for AIS transmissions from ships.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 24, 10:16	6993	0.0013	606	624	96.99	97.99	264	22:30
2023 Feb 13, 05:13	6983	0.0014	595	615	96.79	97.90	15	00:29

Flock 1C-5 2014-033AE 40038						in space
3U Cubesat, part of Planet Labs "Flock 1C" consisting of 11 Earth imaging satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 10:17	6994	0.0013	606	625	97.01	97.99	263
2023 Feb 13, 03:32	6956	0.0011	571	586	96.24	98.04	334

Perseus-M 1 2014-033AF 40039						in space
6U Cubesat (3x2) from Dauria Aerospace equipped with a remote sensing imaging system and a receiver for AIS transmissions from ships.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 24, 10:17	6994	0.0013	607	625	97.01	97.99	257	22:30
2023 Feb 13, 13:04	6984	0.0014	596	616	96.81	97.89	13	00:18

Flock 1C-8 2014-033AG 40040						Re-entered - 2024 Dec 17 Life 3834 days
3U Cubesat, part of Planet Labs "Flock 1C" consisting of 11 Earth imaging satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 11:55	6994	0.0012	607	625	97.02	97.99	257
2023 Feb 13, 03:39	6945	0.0008	562	572	96.00	98.08	306

Flock 1C-3 2014-033AH 40041						Re-entered - 2025 Jan 3 Life 3851 days
3U Cubesat, part of Planet Labs "Flock 1C" consisting of 11 Earth imaging satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 11:55	6994	0.0012	608	624	97.02	97.99	256
2023 Feb 13, 03:16	6953	0.0009	568	581	96.16	98.03	341

PolyITAN 2014-033AJ 40042						in space
1U Cubesat from the National Technical University of Ukraine, equipped with a Sun sensor, orientation system and a GLONASS/GPS navigation system.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 11:55	6994	0.0014	606	626	97.03	97.99	257
2023 Feb 13, 01:59	6968	0.0013	581	599	96.48	98.00	346

TIGRISat 2014-033AK 40043						in space
3U Cubesat for detection of desert dust storms over Iraq - built by Iraqi students at La Sapienza University, Rome. Released from Unisat 6 on June 20 at 21:08:38.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 24, 19:22	7032	0.0062	611	698	97.82	97.98	186
2023 Feb 13, 11:30	7021	0.0060	601	685	97.58	97.66	95

Lemur 1 2014-033AL 40044						in space
3U Cubesat from Nanosatisfi with a technology demonstration payload of visible and IR imagers. Released from Unisat 6 June 20 at 21:07:05 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 25, 01:54	7033	0.0061	612	697	97.82	97.98	185
2023 Feb 13, 05:15	7021	0.0059	602	684	97.59	97.66	99

AeroCube 6a 2014-033AM 40045						in space
0.5U Cubesat from Aerospace Corporation in the US. Released from Unisat 6 June 20 at 21:07:05 simultaneously with ANTELSat, and separated from Aerocube 6 (B) very shortly after. Their joint mission is carrying out inter-satellite communication tests, radiation studies, and testing new attitude sensors. Also acting as a Risk Reduction mission for the forthcoming Aerocube OCSD.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 25, 11:45	7035	0.0061	614	700	97.88	97.98	179
2023 Feb 13, 08:25	7016	0.0057	598	677	97.47	97.66	82

AeroCube 6b 2014-033AN 40046						in space
0.5U Cubesat from Aerospace Corporation in the US. Released from Unisat 6 June 20 at 21:07:05 simultaneously with ANTELSat, and separated from Aerocube 6 (A) very shortly after. Their joint mission is carrying out inter-satellite communication tests, radiation studies, and testing new attitude sensors. Also acting as a Risk Reduction mission for the forthcoming Aerocube OCSD.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 25, 00:20	7035	0.0061	614	700	97.88	97.98	181

Dnepr upper stage 2014-033AP 40047						in space
Launched cluster of 37 satellites. Another satellite - BRITE-Montreal is still attached after it failed to respond to the separation command. Performed a collision avoidance manoeuvre after satellite releases.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 21, 04:05	7409	0.0570	609	1454	105.79	97.90	187

2014-034 PSLV-CA (PSLV C-23) Satish Dhawan Space Centre						2014 Jun 30, 04:22
SPOT 7 (Satellite Pour Observation de la Terre) 2014-034A 40053						in space
Imaging satellite to be operated commercially for the French government. Separated from the launch vehicle at 04:39 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 30, 20:01	7030	0.0012	643	660	97.77	98.26	262	10:00
2023 Feb 13, 10:14	7076	0.0001	697	699	98.73	98.22	80	09:59

AISat 2014-034B 40054						in space
Small satellite, based on Cubesat components as an inexpensive construction method. Built by Germany's DLR to monitor AIS (Automatic Information System) transmissions from shipping, also equipped with a directional aerial to receive AIS-SART (AIS Search and Rescue Transmitter) transmissions from distress beacons. Separated from the launch vehicle at 04:40 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jun 30, 20:01	7030	0.0012	643	660	97.76	98.25	263
2023 Feb 13, 12:54	7003	0.0011	617	632	97.20	98.37	264

CanX-4 (NLS 7.1) 2014-034C 40055						in space
One of a pair of simultaneously-launched, identical small satellites in a project co-ordinated by University of Toronto Institute for Aerospace Studies (UTIAS) Space Flight Laboratory. Their purpose is to demonstrate formation flying by a pair of nanosatellites - each is equipped with a cold gas thrusterand a GPS receiver. Separated from the launch vehicle at 04:41 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 30, 18:23	7029	0.0012	642	659	97.74	98.26	280	10:00
2023 Feb 13, 09:28	7020	0.0013	633	651	97.56	98.38	315	16:46

CanX-5 (NLS 7.2) 2014-034D 40056						in space
One of a pair of simultaneously-launched, identical small satellites in a project co-ordinated by University of Toronto Institute for Aerospace Studies (UTIAS) Space Flight Laboratory. Their purpose is to demonstrate formation flying by a pair of nanosatellites - each is equipped with a cold gas thrusterand a GPS receiver. Separated from the launch vehicle at 04:41 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 30, 16:45	7028	0.0009	643	656	97.72	98.26	295	10:00

Velox 1 2014-034E 40057						in space
Small satellite from Singapore's Nanyang Technological University. Part of its purpose was to give students experience in mounting a satellite building and launch campaign. It carries a high resolution camera for Earth imaging. It will later split into two smaller satellites - N-sat and P-sat to conduct communications experiments. Separated from the launch vehicle at 04:41 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jun 30, 16:45	7027	0.0009	642	655	97.70	98.25	281	10:00
2023 Feb 13, 09:18	7006	0.0010	621	634	97.26	98.37	278	17:55

2014-035 Delta 2 3720 Vandenberg Air Force Base						2014 Jul 2, 09:56
OCO 2 (Orbiting Carbon Observatory) 2014-035A 40059						in space
NASA mission to study carbon dioxide in the atmosphere and make space-based measurements of atmospheric carbon dioxide as a greenhouse gas. OCO will travel about 15 minutes ahead of the existing 'A Train' of Earth observation satellites (GCOM-W1, Aqua, CALIPSO, CloudSat, and Aura) to allow data to be correlated.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jul 4, 20:27	7067	0.0003	687	691	98.55	98.19	122	01:35
2014 Jul 11, 13:29	7064	0.0005	683	689	98.48	98.20	56	01:35
2014 Jul 30, 14:03	7072	0.0000	693	694	98.64	98.20	358	01:36
2014 Aug 4, 14:19	7081	0.0002	701	704	98.83	98.20	88	01:36
2023 Feb 12, 21:32	7081	0.0002	702	704	98.83	98.23	89	01:36

2014-036 Rockot + Briz-KM Plesetsk Cosmodrome						2014 Jul 3, 13:43
Gonets 18 (Gonets M-18) 2014-036A 40061						in space
Store and forward communications satellite for Russia's civil/commercial system. Launched as part of a triple payload. Released from the launch vehicle at 14:28 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 4, 17:13	7873	0.0020	1479	1510	115.87	82.52	313
2014 Aug 21, 01:14	7868	0.0025	1470	1510	115.76	82.51	197
2014 Sep 30, 16:05	7873	0.0030	1471	1518	115.86	82.51	119

Gonets 19 (Gonets M-19) 2014-036B 40062						in space
Store and forward communications satellite for Russia's civil/commercial system. Launched as part of a triple payload. Released from the launch vehicle at 14:28 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 5, 00:57	7874	0.0020	1480	1512	115.89	82.51	316
2014 Sep 23, 23:06	7873	0.0023	1476	1512	115.86	82.50	135

Gonets 20 (Gonets M-20) 2014-036C 40063						in space
Store and forward communications satellite for Russia's civil/commercial system. Launched as part of a triple payload. Released from the launch vehicle at 14:28 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 5, 00:57	7872	0.0020	1478	1509	115.84	82.51	308
2014 Aug 22, 13:46	7873	0.0021	1478	1511	115.86	82.51	191

2014-037 Soyuz-2.1b + Fregat Baikonur Cosmodrome						2014 Jul 8, 15:58
Meteor M-2 2014-037A 40069						in space
Imaging meteorological satellite carrying a range of weather and climate sensors. Precise launch time 15:58:28 UTC. Separated from the Fregat stage at 16:57 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Jul 10, 03:16	7202	0.0007	819	828	101.37	98.81	73	09:00
2023 Feb 13, 11:08	7201	0.0006	819	827	101.36	98.43	354	06:11

Relek (ICA-FC1) 2014-037B 40070						in space
Russian built satellite to study charged particles in the Earth's radiation belts. The name derives from the Russian phrase "Релятивистские электроны" (Relativistic Electrons). Separated from the Fregat stage at 17:39 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 10, 19:06	7099	0.0138	623	819	99.22	98.38	216
2023 Feb 13, 11:45	7095	0.0135	621	813	99.13	97.99	257

DX-1 (Dauria Experimental 1) 2014-037C 40071						in space
First privately-funded Russian satellite, constructed by Dauria Aerospace carrying an AIS (Automatic Identification System) receiver to monitor ships at sea. Separated from the Fregat stage at 17:41 UTC. Initial association with ID and catalogue number by Nico Janssen using radio Doppler measurement.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 10, 03:34	7009	0.0007	626	636	97.33	98.40	251
2023 Feb 13, 08:37	7000	0.0007	617	626	97.14	98.38	265

SkySat 2 2014-037D 40072						in space
Commercial remote sensing satellite for Skybox Imaging of the USA. It will collect high resolution panchromatic and multispectral images of the Earth. Separated from the Fregat stage at 17:41 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 10, 16:33	7008	0.0005	626	634	97.31	98.40	245

UKube 1 2014-037F 40074						in space
3U Cubesat form the UK Space Agency, built as a space technology demonstrator to show how impacts from cosmic particles can be used to increase the security of satellite communications. Separated from the Fregat stage at 17:41 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 10, 05:10	7006	0.0004	626	631	97.27	98.40	254
2023 Feb 13, 10:11	6986	0.0003	605	610	96.85	98.35	206

AISSat 2 2014-037G 40075						in space
Norwegian satellite carrying an AIS (Automatic Identification System) receiver to monitor maritime traffic in Norwegian and international waters. Separated from the Fregat stage at 17:41 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 11, 03:53	7006	0.0004	625	631	97.27	98.40	271
2023 Feb 13, 06:10	6996	0.0005	614	621	97.05	98.37	281

TechDemoSat 1 2014-037H 40076						in space
UK satellite carrying eight technology tests/experiments including measurement of sea state using radio waves reflected off the ocean surface, monitoring the space environment in the vicinity of the satellte for research into space weather, and activaion of a deOrbitSail, a kapton sail designed to reduce the orbit rapidly and cause re-entry. Separated from the Fregat stage at 17:41 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 10, 05:10	7006	0.0004	625	631	97.27	98.40	274
2023 Feb 13, 03:16	6985	0.0007	602	612	96.83	98.36	24

2014-038 Soyuz ST-B + Fregat-MT (VS-08) Centre Spatiale Guyanaise						2014 Jul 10, 18:55
O3b FM03 2014-038A 40079						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 11, 00:36	14219	0.0002	7838	7844	281.24	0.04	322
2014 Jul 27, 08:08	14444	0.0002	8062	8069	287.93	0.05	194

O3b FM07 2014-038B 40080						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 16, 00:00	14216	0.0005	7831	7845	281.15	0.12	103
2014 Aug 21, 18:00	14444	0.0002	8063	8069	287.93	0.03	170

O3b FM06 2014-038C 40081						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 16, 00:00	14214	0.0006	7827	7844	281.08	0.12	122
2014 Aug 21, 18:00	14444	0.0002	8063	8069	287.93	0.03	165

O3b FM08 2014-038D 40082						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 16, 00:00	14207	0.0009	7815	7842	280.87	0.12	153
2014 Aug 21, 18:00	14444	0.0004	8061	8071	287.93	0.03	165

2014-039 Antares 120 Wallops Flight Facility						2014 Jul 13, 16:52
Orb 2 (SS Janet Voss) 2014-039A 40084						Re-entered - 2014 Aug 17 Life 35 days
Cargo delivery mission to the ISS under the NASA Commercial Orbital Transportation Services (COTS) agreement. Precise launch time - 16:52:14 UTC. Carried the Nanoracks CM4 cubesat cluster for launch from the ISS, consisting of 28 satellites of the Planet Labs Flock 1B, TechEdSat 4, GEARRS, MicroMAS and LambdaSat. Captured by ISS manipulator Jul 16 at 10:37 UTC, docked with Harmony node at 12:53 UTC. Undocked Aug 12 at 09:14 UTC and released into independent orbit at 10:42 UTC. Retro-fire led to destructive re-entry above the southern Pacific Ocean 2014 Aug 17 around 05:11 UTC, any surviving fragments hit the ocean surface about 22 min later.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 13, 20:52	6604	0.0039	201	252	89.03	51.65	122
2014 Jul 14, 13:41	6687	0.0091	248	369	90.69	51.62	135
2014 Jul 14, 19:23	6741	0.0048	331	396	91.81	51.64	142
2014 Jul 15, 04:33	6778	0.0019	387	413	92.56	51.64	181
2014 Jul 15, 10:46	6786	0.0009	402	414	92.72	51.64	359
2014 Jul 16, 07:03	6791	0.0005	409	416	92.81	51.65	215
2014 Jul 16, 08:52	6792	0.0006	410	418	92.85	51.64	295
2014 Aug 16, 04:34	6815	0.0003	435	439	93.31	51.64	26
2014 Aug 17, 06:57	6774	0.0015	386	407	92.48	51.65	349

2014-040 Falcon 9 v1.1 Cape Canaveral Air Force Station						2014 Jul 14, 15:15
Orbcomm OG2 FM-109 2014-040A 40086						in space
Second generation LEO store and forward messaging satellites that include an AIS (Automatic InformationSystem) receiver for collecting messages from shipping. Delayed from May 10 because of an unspecified problem with the Falcon 9 rocket while propellant was being loaded for a test firing of the first stage engines the day before intended launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 15, 14:38	7057	0.0084	620	739	98.34	47.00	52

Orbcomm OG2 FM-107 2014-040B 40087						in space
Second generation LEO store and forward messaging satellites that include an AIS (Automatic InformationSystem) receiver for collecting messages from shipping. Delayed from May 10 because of an unspecified problem with the Falcon 9 rocket while propellant was being loaded for a test firing of the first stage engines the day before intended launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 15, 14:38	7058	0.0085	620	739	98.34	47.00	52

Orbcomm OG2 FM-106 2014-040C 40088						in space
Second generation LEO store and forward messaging satellites that include an AIS (Automatic InformationSystem) receiver for collecting messages from shipping. Delayed from May 10 because of an unspecified problem with the Falcon 9 rocket while propellant was being loaded for a test firing of the first stage engines the day before intended launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 15, 14:38	7058	0.0085	620	740	98.35	47.00	52

Orbcomm OG2 FM-111 2014-040D 40089						in space
Second generation LEO store and forward messaging satellites that include an AIS (Automatic InformationSystem) receiver for collecting messages from shipping. Delayed from May 10 because of an unspecified problem with the Falcon 9 rocket while propellant was being loaded for a test firing of the first stage engines the day before intended launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 15, 14:37	7058	0.0086	619	740	98.35	47.00	52

Orbcomm OG2 FM-104 2014-040E 40090						in space
Second generation LEO store and forward messaging satellites that include an AIS (Automatic InformationSystem) receiver for collecting messages from shipping. Delayed from May 10 because of an unspecified problem with the Falcon 9 rocket while propellant was being loaded for a test firing of the first stage engines the day before intended launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 16, 01:34	7058	0.0086	619	741	98.35	47.01	54

Orbcomm OG2 FM-103 2014-040F 40091						in space
Second generation LEO store and forward messaging satellites that include an AIS (Automatic InformationSystem) receiver for collecting messages from shipping. Launch delayed from May 10 because of an unspecified problem with the Falcon 9 rocket while propellant was being loaded for a test firing of the first stage engines the day before intended launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 15, 14:38	7058	0.0086	620	741	98.36	47.00	52

2014-041 Soyuz-2.1a Baikonur Cosmodrome						2014 Jul 18, 20:50
Photon-M 4 (Foton M-4) 2014-041A 40095						Re-entered - 2014 Sep 1 Life 45 days Returned to Earth
Microgravity research satellite, based on the Zenit reconsat re-entry module and the instrument unit from the Yantar satellite, making it similar to Bion-M. Previous Photon missions used the standard Zenit instrument unit. Payload includes a number of material processing experiments and biological samples. Mission intended to last 60 days but as of Jul 23, Photon was not accepting radio commands. Communication was re-established seven days later but, as a result of the problem, the satellite was not manoeuvred to the intended 550 km circular orbit. September 27 - the State Commission for the flight announced that landing would be September 1, and the re-entry module landed near Orenburg, Russia. Note - Listed here because of similarity in name to previous Bion missions but does not truly belong among the Zenit satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 19, 04:48	6780	0.0222	252	553	92.61	64.88	65
2014 Sep 1, 03:20	6764	0.0204	248	524	92.28	64.88	46

2014-042 Soyuz-U 11A511U Baikonur Cosmodrome						2014 Jul 23, 21:44
Progress M-24M (Progress 7K-TGM №423) 2014-042A 40097						Re-entered - 2014 Nov 19 Life 119 days
Supplies to ISS. Precise launch time 21:44:44 UTC. Docked with the Pirs module Jul 24 at 03:31 UTC. Undocked Oct 27 at 05:38 UTC. Retro-fire for 86 seconds, commencing November 19 at 23:00 UTC, provided Δv 106.88 m/s and led to a destructive re-entry over the southern Pacific Ocean. Any unburnt fragments hit the Ocean surface at 23:46:04 UTC near 42°.7 South, 141°.4 West.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 23, 22:13	6575	0.0011	190	205	88.44	51.63	57
2014 Jul 24, 00:48	6794	0.0006	411	420	92.88	51.64	285
2014 Oct 24, 12:39	6792	0.0002	413	416	92.85	51.65	300
2014 Oct 27, 13:24	6773	0.0030	375	415	92.45	51.65	251
2014 Nov 2, 20:20	6785	0.0046	376	438	92.71	51.65	262

2014-043 Delta 4 Medium+ 4,2 Cape Canaveral Air Force Station						2014 Jul 28, 23:28
USA 253 (GSSAP 1) 2014-043A 40099						in space
One of a pair of Geosynchronous Space Situational Awareness Program satellites caried on the first GSSAP launch, designed to act as a sensor in the US Space Surveillance Network (SSN). It will look at objects in geosynchronous orbit with a view to identifying satellites and differentiating between payloads, rocket bodies and debris. Released into near-geosynchronous orbit July 29 around 06:15 UTC. Orbit information is based on amateur observations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2015 Mar 16, 03:46	42202	0.0005	35805	35843	1437.99	0.10	328	129°.7 W
2015 Oct 9, 15:38	42125	0.0001	35742	35751	1434.05	0.02	121	6°.6 W
2019 Sep 10, 19:15	42165	0.0001	35783	35791	1436.12	0.15	65	77°.9 E
2019 Oct 15, 20:38	42164	0.0001	35781	35790	1436.04	0.08	30	78°.0 E
2023 Feb 13, 09:17	43177	0.0003	36788	36811	1488.14	2.25	11

USA 254 (GSSAP 2) 2014-043B 40100						in space
One of a pair of Geosynchronous Space Situational Awareness Program satellites caried on the first GSSAP launch, designed to act as a sensor in the US Space Surveillance Network (SSN). It will look at objects in geosynchronous orbit with a view to identifying satellites and differentiating between payloads, rocket bodies and debris. Released into near-geosynchronous orbit July 29 around 06:15 UTC. Orbit information is based on amateur observations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2019 Sep 11, 12:00	42120	0.0001	35740	35744	1433.81	0.14	142	156°.1 W
2023 Feb 13, 08:33	42488	0.0003	36096	36124	1452.63	1.54	256

USA 255 (ANGELS) 2014-043C 40101						in space
Automated Navigation and Guidance Experiment for Local Space, a small satellite designed to fly alongside a major payload (the upper stage of the Delta 4 used to launch it) to monitor the local space environment. It also carries an experimental detector similar to those aboard the GSSAP satellites to look at other satellites and rocket bodies. Released into near-geosynchronous orbit July 29 around 06:15 UTC. Orbit information is based on amateur observations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2015 Feb 24, 17:06	42550	0.0012	36122	36223	1455.85	0.28	284
2015 Oct 10, 07:31	42550	0.0010	36128	36216	1455.83	0.55	237
2023 Feb 12, 14:14	42605	0.0014	36166	36287	1458.62	6.33	301

Delta 4 upper stage 2014-043D 40102						in space
Launched the GSSAP/ANGELS satellites and acted as a target for ANGELS.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2015 Oct 14, 08:33	42552	0.0008	36142	36206	1455.93	0.56	241

2014-044 Ariane 5ECA (VA-219) Centre Spatiale Guyanaise						2014 Jul 29, 23:47
ATV 5 (Georges Lemaître) 2014-044A 40103						Re-entered - 2015 Feb 15 Life 201 days
European Space Agency cargo carrier to the ISS, final ATV mission. Precise launch time - 23:47:38 UTC. Separated from the launch vehicle July 30 at 00:50 UTC. Passed 6 km from ISS Aug 8 at 22:45 as test of an updated rendezvous system. Docked with ISS Zarya module Aug 12 at 13:29 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Jul 30, 05:49	6638	0.0012	252	267	89.70	51.63	258
2014 Jul 30, 13:20	6711	0.0005	329	336	91.18	51.65	331
2014 Aug 2, 12:43	6715	0.0003	334	339	91.27	51.64	240
2014 Aug 6, 03:22	6721	0.0002	341	344	91.39	51.65	358
2014 Aug 8, 07:12	6759	0.0027	363	399	92.17	51.55	36
2014 Aug 8, 13:21	6777	0.0001	398	400	92.53	51.64	290
2014 Aug 11, 03:08	6804	0.0006	422	429	93.08	51.65	13

2014-045 Atlas V Cape Canaveral Air Force Station						2014 Aug 2, 03:23
USA 256 (Navstar GPS IIF-07) 2014-045A 40105						in space
Seventh Block 2F, Generation 2 GPS Navsat. Launched at the the opening of an 18 minute window, separated from the launch vehicle at 06:47 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 4, 22:59	26851	0.0001	20471	20476	729.81	54.92	191

2014-046 Falcon 9 v1.1 Cape Canaveral Air Force Station						2014 Aug 5, 08:00
Asiasat 8 2014-046A 40107						in space
Comsat for Asia Satellite Telecommunications Company. To cover the Middle East, southern Asia and the Far East. Released from launch vehicle into geosynchronous transfer orbit at 08:32 UTC. Expected location - 105°.5 east, together with Asiasat 7 and Asiasat 3S.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Aug 5, 21:07	24354	0.7304	187	35765	630.39	24.35	180
2014 Aug 6, 12:49	27823	0.5142	7138	35752	769.78	10.67	181
2014 Aug 8, 12:23	35629	0.1822	22759	35742	1115.47	2.65	181
2014 Aug 11, 12:53	42107	0.0001	35726	35732	1433.16	0.09	195	104°.2 E
2014 Aug 13, 07:02	42165	0.0001	35781	35793	1436.10	0.07	249	105°.3 E
2023 Feb 13, 07:54	42165	0.0002	35780	35794	1436.11	0.01	143	3°.9 W

2014-047 CZ 4C Jiuquan Space Centre						2014 Aug 9, 05:45
Yaogan 20 Outlier 2014-047A 40109						in space
One of two further payloads forming the Yaogan 20 mission, and flying in formation with it. May be similar to the US NOSS triplet formations that orbited at a similar altitude and inclination.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 10, 02:36	7473	0.0012	1086	1104	107.16	63.40	39
2014 Aug 15, 05:40	7438	0.0008	1055	1066	106.41	63.39	354
2014 Sep 4, 04:18	7444	0.0006	1062	1070	106.53	63.41	54
2014 Sep 5, 03:24	7450	0.0007	1066	1077	106.66	63.40	320
2014 Sep 10, 11:43	7468	0.0007	1085	1095	107.05	63.40	8
2023 Feb 13, 14:15	7468	0.0283	879	1301	107.04	63.39	9

Yaogan 20 Follower 2014-047B 40110						in space
One of two further payloads forming the Yaogan 20 mission, and flying in formation with it. May be similar to the US NOSS triplet formations that orbited at a similar altitude and inclination.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 10, 02:36	7473	0.0011	1087	1103	107.16	63.40	38
2014 Aug 18, 10:36	7468	0.0004	1087	1093	107.05	63.40	19
2023 Feb 13, 07:07	7468	0.0282	879	1300	107.04	63.39	9

Yaogan 20 Leader 2014-047C 40111						in space
Remote sensing satellite described as undertaking land resources surveys and crop yield estimation. However, its purpose may be ocean surveillance similar to the US NOSS triplet formations that orbited at a similar altitude and inclination. Placed in the same orbit plane as the Yaogan 9 cluster launched 2010 March.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 10, 02:36	7473	0.0012	1086	1104	107.15	63.40	41
2014 Aug 20, 21:29	7468	0.0005	1087	1094	107.05	63.40	14
2023 Feb 13, 07:06	7468	0.0282	879	1301	107.04	63.39	9

2014-048 Atlas V 401 Vandenberg Air Force Base						2014 Aug 13, 18:30
Worldview 3 2014-048A 40115						in space
US commercial Earth imaging satellite owned by Digital Globe.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Aug 14, 02:03	6991	0.0002	612	614	96.96	97.99	85	10:14
2023 Feb 12, 22:00	6991	0.0003	611	615	96.95	97.83	96	10:29

2014-I16 Hand Launch International Space Station						2014 Aug 18, 14:24
Chasqui 1 1998-067ET 40117						Re-entered - 2015 Jan 15 Life 150 days
Cubesat (1U) from a group of academic centres in Peru, led by Universidad Nacional de Ingeniería. It was developed to demonstrate co-operative satellite development and building between Peruvian Universities and learning institutions. It carries an Earth imaging camera. The launch time is ± 1 min.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 19, 06:31	6791	0.0003	411	415	92.82	51.64	160

2014-049 CZ 4B Taiyuan Space Centre						2014 Aug 19, 03:15
Gaofen 2 2014-049A 40118						in space
Carries a high-resolution optical system. Gaofen 2 will support a civilian remote sensing programme based on LEO and GEO satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Aug 19, 20:30	6998	0.0017	608	632	97.10	98.03	213	10:20
2014 Aug 24, 04:12	7006	0.0011	620	636	97.26	98.02	212	10:20
2023 Feb 13, 10:04	7005	0.0005	624	631	97.25	97.73	250	09:46

BRITE PL 2 (Hevelius) 2014-049B 40119						in space
Small astronomical satellite launched as part of the Polish contribution to the Bright Target Explorer programme. It was built by the Copernicus Astronomical Centre.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Aug 19, 20:31	7000	0.0017	610	633	97.13	98.02	207	10:20

2014-I17 Nanoracks Cubesat Deployer International Space Station						2014 Aug 19, 18:25
Flock 1B-24 1998-067EU 40122						Re-entered - 2015 Mar 15 Life 208 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM4 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 21, 03:28	6792	0.0006	410	418	92.85	51.65	68

Flock 1B-23 1998-067EV 40123						Re-entered - 2015 Mar 4 Life 197 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM4 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 20, 19:47	6792	0.0005	411	418	92.85	51.65	70

2014-I18 Nanoracks Cubesat Deployer International Space Station						2014 Aug 20, 02:06
Flock 1B-26 1998-067EW 40124						Re-entered - 2014 Dec 14 Life 116 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM4 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 20, 18:12	6793	0.0002	413	416	92.86	51.65	63

Flock 1B-25 1998-067EX 40125						Re-entered - 2015 Feb 1 Life 165 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM43 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 20, 19:48	6793	0.0002	413	416	92.86	51.64	49

2014-I19 Nanoracks Cubesat Deployer International Space Station						2014 Aug 20, 09:50
Flock 1B-15 1998-067EY 40126						Re-entered - 2015 Jan 7 Life 140 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM4 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 21, 03:28	6793	0.0006	411	418	92.86	51.64	67

Flock 1B-16 1998-067EZ 40127						Re-entered - 2014 Dec 13 Life 115 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM4 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 21, 03:29	6793	0.0006	411	419	92.86	51.65	66

2014-I20 Nanoracks Cubesat Deployer International Space Station						2014 Aug 21, 13:37
Flock 1B-1 1998-067FA 40131						Re-entered - 2015 Jan 1 Life 133 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Launch delayed by two Earth circuits by need to check for potential problem with Nanoracks deployer. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM4 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 23, 06:25	6792	0.0007	409	418	92.84	51.64	76

Flock 1B-2 1998-067FB 40132						Re-entered - 2015 Mar 14 Life 205 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Launch delayed by two Earth circuits by need to check for potential problem with Nanoracks deployer. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM4 cubesat cluster.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 22, 01:14	6792	0.0007	409	419	92.85	51.64	58

2014-050 Soyuz ST-B + Fregat-MT (VS-09) Centre Spatiale Guyanaise						2014 Aug 22, 12:27
Galileo 5 (Doresa, Galileo FOC FM-01) 2014-050A 40128						in space
One of a pair of dual-launched Galileo FOC (Full Operation Capacity) satellites for the European Space Agency navigation system. Aimed at 22300 km circular orbit with 55° inclination, it was delivered to an incorrect orbit when the Fregat stage of the Soyuz rocket failed to complete its second firing properly. The Fregat was wrongly oriented. An independent enquiry board reported 2014 October that it was due to a design flaw that resulted in freezing of propellant in steering thruster feed lines. Subsequently manoeuvred into an orbit where it could provide a useful service. Navigation signal switched on 2014 Nov 29.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 23, 07:10	26198	0.2328	13721	25919	703.34	49.69	25
2014 Nov 5, 13:10	26203	0.2328	13724	25925	703.52	49.73	28
2014 Nov 7, 12:04	26251	0.2305	13821	25924	705.45	49.72	28
2014 Nov 24, 22:00	27979	0.1562	17231	25971	776.25	49.78	29

Galileo 6 (Milena, Galileo FOC FM-02) 2014-050B 40129						in space
One of a pair of dual-launched Galileo FOC (Full Operation Capacity) satellites for the European Space Agency navigation system. Aimed at 22300 km circular orbit with 55° inclination, it was delivered to an incorrect orbit when the Fregat stage of the Soyuz rocket failed to complete its second firing properly. The Fregat was wrongly oriented. An independent enquiry board reported 2014 October that it was due to a design flaw that resulted in freezing of propellant in steering thruster feed lines. Subsequently manoeuvred into an orbit where it could provide a useful service. Navigation signal switched on 2015 March.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 22, 23:07	26182	0.2331	13702	25906	702.69	49.69	25
2015 Jan 19, 16:15	26192	0.2330	13711	25918	703.11	49.77	32
2015 Jan 22, 14:33	26242	0.2307	13810	25918	705.11	49.77	32
2015 Mar 3, 10:00	27977	0.1561	17231	25967	776.19	49.81	34

2014-I21 Nanoracks Cubesat Deployer International Space Station						2014 Aug 23, 19:43
Flock 1B-8 1998-067FC 40133						Re-entered - 2015 Mar 5 Life 194 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM4 cubesat cluster. NASA reported that, along with Flock 1B-8, it "deployed spontaneously" having failed to leave the Nanoracks container when commanded on August 22.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 24, 10:43	6792	0.0008	409	420	92.85	51.64	73

Flock 1B-7 1998-067FD 40134						Re-entered - 2015 Jan 20 Life 150 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM4 cubesat cluster. NASA reported that, along with Flock 1B-7, it "deployed spontaneously" having failed to leave the Nanoracks container when commanded on August 22.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Aug 24, 10:43	6792	0.0008	409	420	92.85	51.65	72

2014-051 CZ 2D Jiuquan Space Centre						2014 Sep 4, 00:15
Ling Qiao 2014-051A 40136						in space
Test satellite for multimedia communications, developed by Beijing Xinwei Telecom Technology Co and Tsinghua University.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Sep 4, 15:11	7171	0.0020	779	808	100.73	98.47	225	06:31
2023 Feb 13, 10:44	7171	0.0022	777	808	100.71	98.63	147	04:44

Chuangxin 1-04 (Innovation 1D) 2014-051B 40137						in space
Small store-dump communications satellite developed by the Chinese Academy of Sciences, it will be used to collect and relay water conservancy, hydrological and meteorological data and data for power supply and disaster relief from remote monitoring stations.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Sep 4, 04:43	7172	0.0022	778	809	100.74	98.46	228	06:31
2023 Feb 13, 09:28	7171	0.0023	776	809	100.72	98.63	148	04:44

2014-I22 Nanoracks Cubesat Deployer International Space Station						2014 Sep 5, 09:29
Flock 1B-18 1998-067FE 40139						Re-entered - 2015 Jan 16 Life 133 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM4 cubesat cluster. Launched spontaneously, along with Flock 1B-17, after several hours of failed commands.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Sep 6, 03:11	6792	0.0007	409	418	92.84	51.65	97

Flock 1B-17 1998-067FF 40140						Re-entered - 2015 Mar 4 Life 180 days
3U Cubesat, part of Planet Labs "Flock 1B" consisting of 28 Earth imaging satellites. Carried to ISS by Cygnus Orb 2 (2014-039A/40084) as part of the Nanoracks CM4 cubesat cluster. Launched spontaneously, along with Flock 1B-18, after several hours of failed commands.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Sep 5, 19:21	6792	0.0007	409	418	92.84	51.65	98

2014-052 Falcon 9 v1.1 Cape Canaveral Air Force Station						2014 Sep 7, 05:00
Asiasat 6 2014-052A 40141						in space
Comsat for Asia Satellite Telecommunications Company to cover Asia, Australia, India and the Pacific islands. Released from the launch vehicle into geosynchronous transfer orbit at 05:32 UTC. Expected location - 120° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Sep 7, 09:27	24343	0.7318	151	35779	629.96	25.33	180
2014 Nov 3, 12:19	42166	0.0001	35783	35793	1436.17	0.07	180	120°.0 E
2023 Feb 11, 23:48	42164	0.0001	35783	35790	1436.07	0.06	38	119°.9 E

2014-053 CZ 4B Taiyuan Space Centre						2014 Sep 8, 03:22
Yaogan 21 2014-053A 40143						in space
Described as being used for remote sensing but mission is probably military or government photo-reconnaissance. Replacement for Yaogan 12.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Sep 8, 12:50	6865	0.0010	480	494	94.35	97.42	260	10:30
2023 Feb 13, 14:03	6872	0.0013	485	503	94.49	97.32	98	09:53
2023 Aug 3, 09:30	6874	0.0010	489	503	94.53	97.30	195	09:45

Tiantuo 2 2014-053B 40144						Re-entered - 2025 Feb 1 Life 3799 days
Small satellite from China's National University of Defense Technology including experimental/test equipment, a real-time video based Earth imaging system, and an AIS receiver for relaying ship location information from the worlds' oceans. Catalogue Number and Designation subject to confirmation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Sep 8, 14:27	6863	0.0012	477	493	94.31	97.42	274	10:30
2023 Feb 13, 08:10	6820	0.0011	434	449	93.41	97.17	53	10:46
2023 Aug 3, 11:26	6806	0.0010	421	434	93.12	97.16	138	10:46

2014-054 Ariane 5ECA (VA-218) Centre Spatiale Guyanaise						2014 Sep 11, 22:05
Optus 10 2014-054A 40146						in space
Comsat to provide high quality broadcast services to households, and twoway voice and data communication services to remote areas around Australasia. Launched 44 minutes into a 62 minute launch window. Expected location - 164° east, test location 176° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Sep 12, 04:04	24379	0.7277	260	35740	631.35	5.94	178
2014 Sep 14, 13:36	27547	0.5298	6575	35763	758.36	2.87	178
2014 Sep 14, 19:46	32902	0.2807	17287	35760	989.89	0.97	177
2014 Sep 16, 13:59	40821	0.0324	33118	35767	1367.98	0.07	152
2014 Sep 18, 07:32	42134	0.0005	35734	35778	1434.52	0.06	42	175°.0 E
2014 Sep 22, 11:29	42164	0.0004	35767	35804	1436.05	0.06	172	176°.1 E
2014 Oct 16, 17:14	42238	0.0003	35850	35871	1439.86	0.04	209	175°.1 E
2014 Oct 30, 20:20	42165	0.0004	35772	35802	1436.11	0.05	160	164°.0 E
2023 Feb 13, 00:11	42165	0.0002	35778	35796	1436.11	0.07	30	156°.0 E

MEASAT 3b 2014-054B 40147						in space
Comsat covering Malaysia, Indonesia, South Asia and Australia. Launched 44 minutes into a 62 minute launch window. Expected location: 91°.5 east, alongside Measat 3 and Measat 3a.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Sep 12, 04:42	24386	0.7273	273	35742	631.63	5.94	178
2014 Sep 14, 23:32	33822	0.2449	19159	35729	1031.72	1.05	175
2014 Sep 30, 00:50	42165	0.0001	35783	35790	1436.09	0.07	342	84°.5 E
2014 Oct 9, 17:36	42067	0.0002	35680	35697	1431.11	0.05	1	87°.1 E
2014 Oct 16, 23:46	42164	0.0002	35779	35793	1436.07	0.04	4	91°.6 E
2023 Feb 13, 10:05	42165	0.0003	35775	35799	1436.12	0.04	317	91°.5 E

2014-055 Atlas V 401 Cape Canaveral Air Force Station						2014 Sep 17, 00:10
USA 257 (CLIO) 2014-055A 40208						in space
US Government satellite aimed at geosynchronous orbit. The mission is unknown but it may be related to US military activity in the Middle East. Launched during a 146 minute window that opened Sep 16 at 21:44 UTC. Reportedly released from launch vehicle at 03:01 UTC into low inclination transfer orbit probably about 20000 x 36000 km. Orbits listed are based on amateur visual observation.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2015 Jun 25, 16:43	42174	0.0014	35737	35854	1436.55	0.04	318	105°.8 E

2014-056 Falcon 9 v1.1 Cape Canaveral Air Force Station						2014 Sep 21, 05:52
SpaceX Dragon CRS-4 2014-056A 40210						Re-entered - 2014 Oct 25 Life 34 days Returned to Earth
Carrying a cargo to the ISS under NASA's Commercial Resupply Services (CRS) contract, including the ISS-RapidScat instrument as a replacement for NASA's QuikScat satellite (1999-034A/25789) to monitor ocean winds for climate research, weather predictions, and hurricanes. Launch attempt September 20 was called off due to bad weather in the final stages of countdown. Captured by ISS Remote Manipulator System Sep 23 at 10:52 UTC, docked with lower port of the Harmony node at 13:27 UTC - retaining bolts were driven home 3-4 minutes later. Undocked from Harmony Oct 25 and released into independent orbit at 13:57 UTC. Retro-fire at 18:43 UTC led to splashdown in Pacific Ocean near 33°.25 N 122°.79 W at 19:38 UTC ±1 min.The launching rocket was not catalogued because it was caused to re-enter above the Indian Ocean about 2.5 hrs after launch.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Sep 21, 10:47	6655	0.0111	203	351	90.05	51.65	48
2014 Sep 22, 11:47	6636	0.0086	201	315	89.66	51.64	56
2014 Sep 23, 06:38	6778	0.0066	355	444	92.55	51.57	152
2014 Sep 23, 08:18	6791	0.0001	412	414	92.82	51.65	129
2014 Oct 25, 16:42	6785	0.0007	403	412	92.71	51.64	18

2014-057 Soyuz-FG 11A511U-FG Baikonur Cosmodrome						2014 Sep 25, 20:25
Soyuz TMA-14M (Soyuz 11F732A47 № 714) 2014-057A 40246						Re-entered - 2015 Mar 12 Life 168 days Returned to Earth
Crew to ISS - Alexander Samokutyaev, Yelena Serova and Barry Wilmore. The port-side solar panel failed to open at launch but was subsequently released shortly after docking with the ISS, possibly as a result of jarring from the docking impact or thermal stresses resulting from the changing sun angle around the ISS orbit. Docked with the port on the Poisk module September 26 at 02:11 UTC. The initial orbit shown is an estimate based on data released by TsUP. Undocked 2015 Mar 11 and 22:44 UTC carrying Samokutayev, Serova and Wilmore. Touched down at at 02:15 UTC 147 km from the town Dzhezkazgan in Kazakhstan.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Sep 25, 20:13	6598	0.0033	198	241	88.89	51.65	76
2014 Sep 26, 05:40	6793	0.0002	413	416	92.86	51.65	124

2014-058 Proton-M + Briz-M Baikonur Cosmodrome						2014 Sep 27, 20:23
Luch (Olympus) 2014-058A 40258						in space
Mission obscure but may be be a combined communications payload (Luch) for use by satellites in LEO, and an electronic intelligence gathering ELINT payload (Olympus) - possibly for the Security Service of the Russian Federation (FSB). It also carries a payload that provides a reference signal to increase navigational accuracy for GLONASS users. The Briz-M stack separated from the Proton third stage at 20:32 UTC. Luch separated from the Briz-M Sep 28 at 05:26 UTC. Before launch there were indications that it was heading for 95° east but it has occupied several different locations for brief periods of time, interspersed with period of drift, maybe as a test of effectiveness.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Sep 29, 22:10	42055	0.0021	35589	35765	1430.50	0.01	92	56°.8 E
2014 Oct 6, 13:27	42103	0.0020	35640	35810	1432.94	0.02	138	65°.7 E
2014 Oct 8, 00:27	42213	0.0025	35730	35940	1438.55	0.02	140	65°.5 E
2014 Oct 10, 14:54	42309	0.0017	35858	36003	1443.47	0.03	171
2014 Oct 19, 20:47	42165	0.0001	35781	35793	1436.12	0.05	9	54°.0 E
2015 Jan 2, 02:37	42165	0.0000	35785	35789	1436.11	0.04	67	52°.9 E
2015 Feb 3, 22:52	41905	0.0001	35523	35530	1422.84	0.02	344
2015 Feb 22, 12:38	42167	0.0000	35788	35789	1436.19	0.06	272	96°.4 E
2015 Apr 7, 20:02	42272	0.0013	35838	35950	1441.59	0.04	183
2015 May 19, 20:17	42316	0.0024	35836	36040	1443.84	0.03	232
2015 Jun 25, 07:06	42165	0.0001	35782	35792	1436.10	0.03	131	18°.1 W
2015 Sep 28, 05:24	42245	0.0005	35844	35889	1440.18	0.05	344
2015 Oct 5, 09:00	42168	0.0002	35780	35798	1436.24	0.05	282	24°.3 W
2023 Feb 12, 09:28	42165	0.0001	35782	35791	1436.09	0.01	228	18°.1 W

2014-059 CZ 2C Jiuquan Space Centre						2014 Sep 28, 05:13
Shijian 11-07 (Practice 11-07) 2014-059A 40261						in space
Reported as an "experimental satellite". The orbit, and images of one of its predecessors, indicate that it has an Earth observation rôle. Launch was brought forward from Sep 29 because of forecast high winds in the launch area.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Sep 28, 12:53	7074	0.0013	687	705	98.69	98.12	198	11:30
2023 Feb 13, 10:33	7069	0.0012	682	699	98.58	98.11	28	10:57

2014-060 H-IIA 202 (F-25) Tanegashima Space Centre						2014 Oct 7, 05:16
Himawari 8 2014-060A 40267						in space
Japanese meteorological imaging and data collection satellite in geosynchronous orbit. Separated from the launch vehicle at 05:43 UTC. Expected location - 140° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Oct 7, 00:34	24443	0.7289	248	35882	633.86	22.33	179
2014 Oct 7, 22:28	28349	0.4907	8060	35881	791.70	8.18	180
2014 Oct 9, 18:48	40171	0.0510	31745	35840	1335.44	0.40	179
2014 Oct 17, 19:26	42164	0.0003	35774	35797	1436.06	0.08	37	140°.8 E
2023 Feb 13, 10:19	42164	0.0001	35782	35790	1436.08	0.04	73	140°.7 E

2014-061 PSLV-XL (PSLV C-26) Satish Dhawan Space Centre						2014 Oct 15, 20:02
IRNSS 1C (Indian Regional Navigation Satellite System 1C) 2014-061A 40269						in space
Satellite in the Indian Regional Navigation Satellite System, located in equatorial geosynchronous orbit - previous launches were to inclined GEO. Separated from the launch vehicle at 20:22 UTC. Expected location 83° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Oct 16, 13:36	16813	0.6045	272	20597	361.58	17.86	179
2014 Oct 16, 22:22	24392	0.7252	324	35704	631.88	17.97	180
2014 Oct 20, 23:55	42080	0.0017	35629	35774	1431.76	4.99	341	74°.3 E
2014 Oct 28, 14:19	42111	0.0016	35665	35800	1433.33	4.97	20	81°.6 E
2014 Oct 31, 22:05	42159	0.0021	35690	35871	1435.80	4.96	355	82°.9 E
2023 Feb 12, 19:18	42165	0.0017	35716	35857	1436.10	3.49	5	83°.0 E

2014-062 Ariane 5ECA (VA-220) Centre Spatiale Guyanaise						2014 Oct 16, 21:43
Intelsat 30 (Intelsat DLA-1) 2014-062A 40271						in space
DLA 1 (Direct Latin America 1) will provide direct communications services to homes on the SW coast of the US, across some of South America and part of the Caribbean Sea. Separated from the launch vehicle at 22:01 UTC. Expected location - 95° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Oct 17, 14:38	24401	0.7278	265	35781	632.23	5.97	178
2014 Oct 19, 10:15	27185	0.5507	5837	35776	743.44	3.09	178
2014 Oct 20, 17:29	31963	0.3190	15388	35782	947.84	1.60	180
2014 Oct 20, 21:39	38440	0.0970	28332	35792	1250.06	0.31	162
2014 Oct 21, 07:42	40882	0.0325	33173	35834	1371.04	0.17	150
2014 Oct 23, 18:11	42022	0.0045	35454	35833	1428.80	0.07	64	134°.7 W
2014 Oct 27, 00:57	42169	0.0021	35703	35878	1436.32	0.04	109	132°.1 W
2014 Nov 9, 15:52	42018	0.0002	35632	35648	1428.61	0.04	47	130°.2 W
2014 Nov 11, 09:39	41868	0.0002	35479	35500	1420.94	0.03	311
2014 Nov 17, 23:33	42006	0.0002	35621	35636	1428.01	0.04	7	98°.8 W
2014 Nov 21, 16:22	42162	0.0002	35776	35793	1435.97	0.03	234	95°.0 W
2023 Feb 8, 20:45	42165	0.0002	35778	35796	1436.12	0.02	22	95°.1 W

ArSat 1 2014-062B 40272						in space
Argentinian comsat to provide television, telephony and Internet access across Argentina, Chile, Uruguay and Paraguay. Separated from launch vehicle at 22:17 UTC. Expected location - 72° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Oct 17, 14:38	24384	0.7275	266	35746	631.57	5.99	178
2014 Oct 29, 12:16	42166	0.0003	35777	35799	1436.16	0.01	231	79°.4 W
2014 Oct 31, 12:37	42198	0.0010	35777	35862	1437.79	0.01	218	79°.8 W
2014 Nov 4, 17:42	42164	0.0000	35785	35787	1436.07	0.02	153	81°.1 W
2014 Nov 24, 18:35	42120	0.0001	35737	35746	1433.81	0.02	277	79°.0 W
2014 Dec 11, 12:42	42164	0.0002	35778	35795	1436.07	0.01	236	71°.8 W
2023 Feb 13, 04:41	42165	0.0001	35781	35792	1436.10	0.04	33	71°.8 W

2014-063 CZ 4C Taiyuan Space Centre						2014 Oct 20, 06:31
Yaogan 22 2014-063A 40275						in space
Described as being used for remote sensing for natural resources surveys. Specific tasks include land survey, crop yield assessment, and input to disaster monitoring and prevention plans. Mission is probably military or government photo-reconnaissance.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Oct 20, 07:44	7581	0.0008	1196	1209	109.48	100.32	127	13:29
2023 Feb 12, 07:13	7580	0.0006	1197	1207	109.47	100.59	67	13:46

2014-064 Proton-M + Briz-M Baikonur Cosmodrome						2014 Oct 21, 15:09
Express-AM6 2014-064A 40277						in space
Russian domestic communications satellite to carry mobile presidential and governmental communications, digital television, radio broadcasting and multimedia services and VSAT networks. Precise launch time, 15:09:32 UTC. Separated from the launch vehicle Oct 22 at 00:31:26 UTC but into an orbit that may have been slightly lower than intended. Data published in respect of the Briz-M firings suggested that it may have under-performed, something later confirmed by Roscosmos. Used its own electric thrusters over a period of weeks to move towards its planned orbit. Entered geosynchronous drift orbit 2014 Dec 1. Expected location - 53° east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Oct 25, 04:44	40926	0.0792	31306	37790	1373.28	0.70	359
2014 Nov 10, 00:16	40994	0.0780	31417	37815	1376.71	0.68	359
2014 Nov 19, 23:42	41595	0.0787	31944	38490	1407.09	0.64	1
2014 Dec 1, 15:21	42243	0.0776	32588	39142	1440.12	0.63	1
2015 Jan 15, 00:25	42243	0.0419	34094	37636	1440.09	0.53	3
2015 Mar 5, 23:22	42175	0.0024	35695	35899	1436.63	0.42	14	51°.1 E
2015 Mar 10, 19:21	42164	0.0003	35774	35798	1436.06	0.42	295	50°.9 E
2023 Feb 12, 20:08	42165	0.0000	35785	35788	1436.10	0.05	86	53°.0 E

2014-065 CZ 3C/2 Xichang Space Centre						2014 Oct 23, 18:00
Chang'e 5 Test Vehicle 2014-065A 40283						in space
Engineering test mission for components of a Lunar sample return mission. At about 18:20 UTC, the CZ-3C upper-stage re-ignited for a 3-4 minute firing to push itself from LEO into a trajectory aimed at the Moon. The test vehicle separated from the launch vehicle at a distance of 5000 km from Earth shortly after engine shut-down. The journey to the Moon and subsequent return to Earth was a full command and control ‘dress rehearsal’ for Chang'e 5 in 2017 including setting up the Earthbound trajectory, conducting mid-course corrections, tracking, atmosphere re-entry and vehicle recovery. The descent vehicle separated from the main spacecraft Oct 31 at 21:52 UTC, entered the Earth's atmosphere and landed on the Siziwang Banner of Inner Mongolia at 22:42 UTC. The main spacecraft then made a thruster firing to ensure that it remained in orbit heading for the Earth-Moon L2 Lagrange Point where it arrived 2014 Nov 27 before returning to the Moon. Entered orbit the Moon 2015 Jan 13. For about three months it conducted engineering tests relating to spacecraft operation in lunar orbit . The initial orbit shown describes the outbound trajectory. The second listed orbit is for the Earth return leg of the mission, it was computed by Cees Bassa.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Oct 23, 14:49	208102	0.9755	-1282	404729	15746.12	30.47	146
2014 Oct 31, 18:18	207948	0.9678	327	402812	15728.59	46.12	23

4M (Manfred Memorial Moon Mission) 2014-065B 40284						Re-entered - 2015 Oct 6 Life 348 days
Payload provided by the company Luxspace, named to commemorate the late Professor Manfred Fuchs. 4M included a radio transmitter, permanently attached to the launch vehicle upper stage, operating in the 2m amateur band designed to operate continuously throughout a complete circuit of the Earth-Moon system and, hopefully, longer. In the event, it fell silent on November 11 when the sun angle on its solar panel was insufficient to provide enough charging current. The orbit shown describes the outbound trajectory towards the Moon.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Oct 23, 14:49	208102	0.9755	-1282	404729	15746.12	30.47	146

2014-066 CZ 2C Jiuquan Space Centre						2014 Oct 27, 06:59
Shijian 11-08 (Practice 11-08) 2014-066A 40286						in space
Reported as an "experimental satellite". The orbit, and images of one of its predecessors, indicate that it has an Earth observation rôle.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Oct 27, 09:43	7074	0.0013	687	705	98.69	98.22	201	13:15
2023 Feb 13, 11:06	7063	0.0014	675	695	98.46	98.19	95	13:38

2014-F02 - failed to reach orbit Antares 130 Wallops Flight Facility						2014 Oct 28, 22:22
Cygnus OA-3 (SS Deke Slayton)
Cargo delivery mission under the NASA Commercial Orbital Transportation Services (COTS) agreement. Precise launch time - 22:22:38 UTC. Carried the Nanoracks CM5 cubesat cluster for launch from the ISS, consisting of 26 satellites of the Planet Labs Flock 1D, GOMX 2, RACE and Arkyd 3. Orb 3 was lost when the Antares rocket suffered a failure within a few seconds of liftoff and crashed on the launch site. Some of the Cubesats were recovered intact from the resulting debris.

2014-067 Soyuz-2.1a Baikonur Cosmodrome						2014 Oct 29, 07:09
Progress M-25M (Progress 7K-TGM №424) 2014-067A 40292						Re-entered - 2015 Apr 26 Life 179 days
Supplies to ISS. Precise launch time 07:09:42 UTC. Docked with the Pirs module at 13:08:15 UTC. Undocked 2015 Apr 25 at 06:41:14 UTC. Retro-fire at Apr 28 at 12:08 UTC led to a destructive re-entry over the southern Pacific Ocean. Any unburnt fragments hit the Ocean surface at around 12:57 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Oct 29, 09:11	6656	0.0030	258	298	90.07	51.65	314
2014 Oct 29, 11:48	6691	0.0073	264	361	90.77	51.65	264
2014 Oct 30, 01:49	6793	0.0004	412	417	92.86	51.64	341

2014-068 Atlas V 401 Cape Canaveral Air Force Station						2014 Oct 29, 17:21
USA 258 (Navstar GPS IIF-08) 2014-068A 40294						in space
Eighth Block 2F, Generation 2 GPS Navsat. Launched at the the opening of an 18 minute window. Separated from the launch vehicle at 17:45 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Nov 3, 13:03	26845	0.0003	20460	20474	729.56	54.97	273
2014 Dec 8, 11:41	26562	0.0011	20155	20211	718.02	54.97	200

2014-069 Soyuz-2.1a + Fregat Plesetsk Cosmodrome						2014 Oct 30, 01:43
Meridian 7 (Meridian № 17L) 2014-069A 40296						in space
HEO military/government comsat to support Russian forces, commercial shipping and communication ground stations at northern latitudes across Russia. Meridian also supports the clandestine short messaging system formerly provided by the Parus satellites.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Oct 30, 14:13	26736	0.7253	967	39749	725.12	62.81	270
2014 Nov 14, 15:17	26558	0.7236	962	39398	717.88	62.82	270

2014-070 Dnepr Dombarovsky (Yasny) Cosmodrome						2014 Nov 6, 07:35
ASNARO 1 (Advanced Satellite with New system ARchitecture for Observation) 2014-070A 40298						in space
Japanese Earth observation satellite created in collaboration between the NEC Corporation and Japan Space Systems uder contract for the Ministry of Economy, Trade and Industry. Precise launch time 07:35:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Nov 6, 21:45	6885	0.0001	506	507	94.75	97.48	95	10:57
2023 Feb 13, 13:55	6885	0.0006	503	512	94.76	97.45	178	11:01

Hodoyoshi 1 2014-070B 40299						in space
Small satellite from the University of Tokyo and NESTRA (Next Generation Space System Technology Association) to produce medium-high resolution Earth images. Precise launch time 07:35:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Nov 6, 21:52	6894	0.0014	506	525	94.93	97.48	181	10:57
2023 Feb 13, 13:26	6853	0.0011	467	483	94.10	97.21	7	09:49

ChubuSat 1 (Kinshachi) 2014-070C 40300						Re-entered - 2025 Jan 16 Life 3724 days
Technology demonstration satellite from Nagoya University and Daido University. It carries an Earth imager, sensors to detect space debris and an amateur radio communications system. Precise launch time 07:35:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Nov 6, 21:53	6900	0.0024	506	538	95.07	97.48	182	10:57
2023 Feb 13, 10:03	6856	0.0017	466	490	94.16	97.16	25	08:47

Qsat-EOS (KYUshu SATellite - Earth Observation System) 2014-070D 40301						Re-entered - 2023 Dec 3 Life 3314 days
Small satellite from Kyushu University with a range of sensors for disaster monitoring in the Kyushu region, observing the Earth's magnetic field, detection of space micro-debris, and observing water vapour in the upper atmosphere. Precise launch time 07:35:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Nov 6, 18:43	6908	0.0034	506	553	95.23	97.47	182	10:57
2023 Feb 13, 13:33	6798	0.0014	410	429	92.96	97.17	315	10:00

TSUBAME 2014-070E 40302						Re-entered - 2024 Nov 5 Life 3652 days
Small satellite for Earth observation and observation of gamma ray bursts from the sky. Precise launch time 07:35:49 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Nov 6, 21:47	6915	0.0046	505	569	95.38	97.47	182	10:57
2023 Feb 13, 14:08	6868	0.0035	466	513	94.40	97.13	83	06:36

2014-071 CZ 2C Taiyuan Space Centre						2014 Nov 14, 18:53
Yaogan 23 2014-071A 40305						Re-entered - 2024 Dec 12 Life 3681 days
Imaging satellite carrying a synthetic aperture radar for natural resources surveys and, possibly, intelligence gathering. Specific tasks include land survey, crop yield assessment, and input to disaster monitoring and prevention plans.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Nov 15, 02:47	6881	0.0015	492	513	94.67	97.33	241	02:00
2014 Nov 16, 08:57	6882	0.0011	496	512	94.70	97.33	240	02:00
2014 Nov 17, 13:17	6891	0.0001	513	514	94.89	97.33	122	01:59
2023 Feb 13, 14:22	6867	0.0003	486	490	94.38	97.64	79	02:45

2014-072 CZ 2D Jiuquan Space Centre						2014 Nov 20, 07:12
Yaogan 24 2014-072A 40310						in space
Described as being used for remote sensing for natural resources surveys. Specific tasks include land survey, crop yield assessment, and input to disaster monitoring and prevention plans. Mission is probably military or government photo-reconnaissance.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Nov 20, 09:54	7020	0.0017	630	653	97.55	97.91	208	13:30
2023 Feb 13, 11:20	7020	0.0016	630	652	97.55	98.00	220	13:35

2014-073 Kuaizhou 1 Jiuquan Space Centre						2014 Nov 21, 06:37
Kuaizhou 1 third stage 2014-073A 40311						Re-entered - 2016 Oct 9 Life 688 days
Small remote sensing satellite intended to assist in disaster monitoring. There is no separately-catalogued upper stage because it is integrated with the satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Nov 21, 18:09	6671	0.0012	285	301	90.37	96.56	281	13:00
2014 Nov 23, 05:10	6668	0.0012	282	298	90.31	96.56	274	12:59
2014 Nov 23, 08:10	6673	0.0009	289	301	90.42	96.56	217	12:59
2014 Dec 1, 03:04	6660	0.0009	276	287	90.15	96.56	217	12:59
2014 Dec 1, 07:25	6684	0.0031	285	326	90.64	96.55	327	12:59
2014 Dec 18, 04:52	6658	0.0028	260	298	90.10	96.56	259	12:58
2014 Dec 18, 13:41	6682	0.0016	293	314	90.59	96.55	13	12:58
2014 Dec 31, 05:05	6665	0.0018	275	299	90.26	96.55	327	12:57
2014 Dec 31, 08:06	6690	0.0025	295	328	90.76	96.54	206	12:57

2014-074 Soyuz-FG 11A511U-FG Baikonur Cosmodrome						2014 Nov 23, 21:01
Soyuz TMA-15M (Soyuz 11F732A47 № 715) 2014-074A 40312						Re-entered - 2015 Jun 11 Life 200 days Returned to Earth
Crew to ISS - Anton Shkaplerov (Roscosmos), Terry Virts (NASA), Samantha Cristoforetti (ESA). Docked with ISS Rassvet module Nov 24 at 02:48:21 UTC. The initial orbit shown is an estimate based on data from TsUP.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Nov 23, 20:49	6590	0.0022	197	226	88.73	51.64	76
2014 Nov 23, 23:05	6691	0.0002	311	314	90.78	51.62	120
2014 Nov 24, 03:18	6791	0.0007	408	417	92.82	51.65	63

2014-I23 SSIKLOPS small satellite deployer International Space Station						2014 Nov 28, 14:30
SpinSat (Special Purpose Inexpensive Satellite) 1998-067FL 40314						Re-entered - 2017 Mar 11 Life 834 days
Small spherical satellite from the US Naval Research Laboratory to test movement and positioning of a small satellite in space using new technology micro-thrusters. It is equipped with an array of electrically-controlled solid propellant thrusters on its surface, and a single axis momentum wheel. It was carried to the ISS by Dragon on the CRS-4 mission (2014-056A/40210), 2014 September.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Nov 29, 00:22	6790	0.0009	406	419	92.81	51.65	73

2014-075 Soyuz-2.1b + Fregat Plesetsk Cosmodrome						2014 Nov 30, 21:52
Cosmos 2501 (Uragan-K1 № 12L) 2014-075A 40315						in space
Second launch of new-design GLONASS-K. It also carries radio receiving equipment for the COSPAS-SARSAT international search and rescue system. Released from the launch vehicle Dec 1 at 01:25 UTC.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 2, 11:57	25519	0.0015	19103	19178	676.15	64.83	247
2014 Dec 22, 05:04	25508	0.0018	19084	19176	675.73	64.82	242

2014-076 H-IIA 202 (F-26) Tanegashima Space Centre						2014 Dec 3, 04:22
Hayabusa 2 2014-076A 40319						Re-entered - 2020 Dec 5 Life 2194 days
Japanese Minor Planet sample return mission. Precise launch time - 04:22:04 UTC, released from the launch vehicle at 05:59:25 UTC. An Earth swing-by 2015 December 3 set the vehicle on course for rendezvous 2018 June 27 with Minor Planet (162173) 1999 JU₃, Ryugu. It release four smaller probes to help investigate the surface. Experiments included creation of an artificial crater and collection of a surface sample from the resulting debris cloud. Departed Ryugu 2019 Dec 13 for return to Earth. Re-entry vehicle containing the soil sample separated 2020 Dec 5 and the main vehicle continued on an Earth swing-by trajectory. Sample container entered the Earth's atmosphere Dec 5 and landed near Woomera, Australia shortly before 18:00 UTC after a parachute descent. It was locate later the same day for subsequent recovery.
Heliocentric orbit

Shin’en 2 2014-076B 40320						in space
Small space vehicle carrying an amateur radio payload as a test of long distance communications. Signals were tracked up to 2014 Dec 8 when the vehicle was 2.3 million km from Earth.
Heliocentric orbit

ARTSAT 2: DESPATCH 2014-076C 40321						in space
Encased in a sculptured artwork, the vehicle carries an experiment in receiving very weak signals sent from space to a worldwide array of receiving stations It is also testing the use of 3D-printed parts (the sculpture) for spacecraft. Final signals received 2015 Jan 3 from a distance of 4.7 million km when the batteries ran down.
Heliocentric orbit

PROCYON (Proximate Object Close flyby with Optical Navigation) 2014-076D 40322						in space
Technology demonstrator for a deep space mission built by the University of Tokyo aimed at Minor Planet 2000 DP107. Payload included an optical navigation system for use in vicinity of its target. The onboard ion thruster operated but not as planned and, early-mid 2015, the mission was abandoned.
Heliocentric orbit

H-IIA upper stage 2014-076E 40323						in space
Launched Hayabusa 2 and three smaller spacecraft.
Heliocentric orbit

2014-077 Delta 4 Heavy Cape Canaveral Air Force Station						2014 Dec 5, 12:05
Orion Exploration Flight Test 1 2014-077A 40329						Re-entered - 2014 Dec 5 Life <1 day
Test flight of the Orion spacecraft in the development programme for a new NASA crew carrier. Landed in the Pacific Ocean about 1000 km SW of San Diego, California at 16:29 UTC. Orbit shown is after the second firing of of the Delta 4 upper stage - it produced the high apogee and ensured re-entry without the need for further retro-fire.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 5, 16:09	9259	0.3147	-33	5795	147.78	28.76	137

2014-078 Ariane 5ECA (VA-221) Centre Spatiale Guyanaise						2014 Dec 6, 20:40
GSat 16 2014-078A 40332						in space
Indian communication satellite to provide public and private television and radio services, and large-scale Internet and telephone operations. Coverage includes the Indian mainland, Sri Lanka, the Maldives, and the Andaman-Nicobar Islands. Separated from the launch vehicle at 21:12 UTC. It will initially work alongside, and then replace, GSat 3E at 55° East.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Dec 7, 02:05	24341	0.7284	233	35692	629.88	6.10	179
2014 Dec 8, 18:18	32265	0.3065	15998	35775	961.28	1.06	172
2014 Dec 11, 17:55	42102	0.0045	35534	35914	1432.91	0.19	124	46°.4 E
2014 Dec 16, 15:28	42067	0.0024	35589	35789	1431.11	0.18	127	53°.3 E
2014 Dec 19, 21:17	42165	0.0003	35776	35798	1436.10	0.18	201	55°.1 E
2023 Feb 13, 04:45	42164	0.0003	35773	35799	1436.07	0.13	177	55°.1 E

DirecTV 14 2014-078B 40333						in space
Broadcast satellite to provide digital TV services to users across the Continental US, Hawaii, Alaska and Puerto Rico. Separated from the launch vehicle at 21:07 UTC. Expected location - 99° west.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Dec 7, 02:11	24380	0.7285	241	35762	631.39	6.01	178
2014 Dec 8, 17:33	27496	0.5337	6443	35792	756.24	3.09	179
2014 Dec 9, 12:20	33307	0.2646	18115	35742	1008.22	1.63	174
2014 Dec 10, 12:13	33760	0.2493	18967	35797	1028.88	1.08	178
2014 Dec 11, 16:26	41226	0.0229	33905	35790	1388.38	0.10	160
2014 Dec 13, 04:15	42150	0.0004	35756	35787	1435.33	0.08	166	76°.4 W
2014 Dec 17, 07:43	42165	0.0001	35783	35791	1436.12	0.07	162	76°.0 W
2015 Jan 13, 15:40	42310	0.0000	35930	35933	1443.51	0.02	46
2015 Jan 29, 14:28	42165	0.0000	35786	35787	1436.11	0.01	302	99°.3 W
2023 Feb 12, 07:21	42165	0.0001	35783	35790	1436.09	0.02	122	99°.3 W

2014-079 CZ 4B Taiyuan Space Centre						2014 Dec 7, 03:26
CBERS 4 (Ziyuan-1 04, China-Brazil Earth Resources Satellite) 2014-079A 40336						in space
China-Brazil Earth Resouces Satellite carrying a range of Earth observation sensors. Separated from the launch vehicle at 03:38 UTC. Launch brought forward by 12 months after CBERS 3 failed to reach orbit 2013 December.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Dec 7, 12:51	7121	0.0007	738	748	99.67	98.55	263	10:30
2023 Feb 13, 10:50	7152	0.0002	772	775	100.32	98.46	90	10:23

2014-080 CZ 4C Jiuquan Space Centre						2014 Dec 10, 19:33
Yaogan 25 Leader 2014-080A 40338						in space
Remote sensing satellite described as undertaking land resources surveys and crop yield estimation. However, its purpose may be ocean surveillance similar to the US NOSS triplet formations that orbited at a similar altitude and inclination. Placed in the same orbit plane as the Yaogan 16 cluster launched 2012 Nov.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 11, 03:54	7471	0.0005	1089	1097	107.12	63.41	2
2014 Dec 14, 16:41	7462	0.0008	1078	1090	106.91	63.41	228
2015 Jan 6, 01:55	7466	0.0010	1080	1094	106.99	63.41	215
2015 Jan 7, 15:23	7468	0.0013	1081	1100	107.05	63.41	229
2023 Feb 12, 21:42	7468	0.0258	897	1282	107.04	63.40	4

Yaogan 25 Trailer 2014-080B 40339						in space
One of two further payloads forming the Yaogan 25 mission, and flying in formation with it. May be similar to the US NOSS triplet formations that orbited at a similar altitude and inclination.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 11, 03:54	7472	0.0004	1091	1097	107.14	63.41	358
2014 Dec 13, 13:02	7466	0.0006	1083	1093	107.01	63.42	255
2014 Dec 14, 19:44	7463	0.0009	1077	1091	106.93	63.41	241
2015 Jan 7, 10:04	7462	0.0008	1079	1090	106.93	63.41	242
2015 Jan 7, 11:51	7464	0.0007	1080	1090	106.95	63.41	235
2015 Jan 8, 09:49	7466	0.0010	1080	1096	107.00	63.41	245
2015 Jan 9, 10:29	7468	0.0012	1081	1099	107.05	63.41	226

Yaogan 25 Outlier 2014-080C 40340						in space
One of two further payloads forming the Yaogan 25 mission, and flying in formation with it. May be similar to the US NOSS triplet formations that orbited at a similar altitude and inclination.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 11, 11:03	7472	0.0004	1091	1097	107.14	63.41	350
2014 Dec 12, 15:53	7480	0.0014	1092	1113	107.31	63.40	36
2014 Dec 14, 11:16	7491	0.0004	1110	1116	107.54	63.42	39
2015 Jan 1, 01:34	7491	0.0007	1108	1118	107.54	63.41	33
2015 Jan 6, 19:35	7491	0.0008	1107	1119	107.54	63.41	32
2015 Jan 7, 10:13	7487	0.0002	1107	1111	107.45	63.41	20
2015 Jan 9, 05:25	7471	0.0012	1084	1101	107.10	63.40	242
2015 Jan 11, 01:27	7468	0.0013	1081	1100	107.05	63.41	231
2023 Feb 12, 21:42	7468	0.0257	898	1282	107.04	63.39	4

2014-081 Atlas V 541 Vandenberg Air Force Base						2014 Dec 13, 03:19
USA 259 (SIGINT/SBIRS) 2014-081A 40344						in space
Multi-tasking satellite for US National Reconnaissance Office, probably including electronic intelligence gathering and missile launch detection using SBIRS (Space-Based Infra Red System). The orbits are derived from amateur visual observation. The Centaur stage of the rocket was caused to re-enter above the Southern Ocean a little over 10 hours after lift-off.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 16, 06:15	26303	0.6776	2103	37746	707.55	62.85	267
2015 Jan 30, 17:46	26556	0.6788	2152	38204	717.82	62.83	267

2014-082 Proton-M + Briz-M Baikonur Cosmodrome						2014 Dec 15, 00:16
Yamal 401 2014-082A 40345						in space
Russian domestic communications satellite. Separated from the launch vehicle at 09:17 UTC. Expected location: 90° east. The first four sets of orbit parameters are based on data published by Khrunichev.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Dec 15, 00:31	6560	0.0011	174	189	88.12	51.55	80
2014 Dec 15, 01:41	9008	0.2627	264	4996	141.81	49.65	359
2014 Dec 15, 04:03	24389	0.7222	397	35625	631.76	47.67	359
2014 Dec 15, 09:16	41877	0.0032	35364	35635	1421.44	0.06	179
2014 Dec 16, 07:58	41870	0.0035	35344	35640	1421.07	0.04	201
2015 Jan 5, 17:36	42169	0.0007	35761	35822	1436.33	0.03	242	89°.9 E
2023 Feb 12, 06:03	42165	0.0001	35782	35791	1436.09	0.01	347	90°.0 E

2014-083 Soyuz ST-B + Fregat-MT (VS-10) Centre Spatiale Guyanaise						2014 Dec 18, 18:37
O3b FM10 2014-083A 40348						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 18, 22:25	14218	0.0003	7836	7844	281.21	0.04	318
2015 Jan 7, 07:09	14444	0.0002	8063	8068	287.93	0.04	300

O3b FM11 2014-083B 40349						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 19, 02:57	14213	0.0002	7832	7837	281.04	0.04	122
2015 Jan 7, 07:09	14444	0.0002	8063	8069	287.93	0.04	288

O3b FM12 2014-083C 40350						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 19, 02:57	14208	0.0009	7818	7842	280.91	0.04	156
2015 Jan 7, 07:09	14444	0.0002	8063	8069	287.93	0.04	288

O3b FM09 2014-083D 40351						in space
Communications satellite, owned by O3b Networks, to provide broadband links between ground stations lying in the range ±45° latitude. Orbiting at one quarter the altitude of geosynchronous satellites, O3b satellites reduce the delays (latency) in transmission introduced by the lengths of radio links.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 18, 22:33	14210	0.0003	7827	7836	280.95	0.03	149
2015 Jan 7, 07:09	14444	0.0002	8063	8069	287.93	0.04	297

2014-084 Strela Baikonur Cosmodrome						2014 Dec 19, 04:43
Condor-E № 2 2014-084A 40353						Re-entered - 2022 Oct 22 Life 2864 days
Small satellite for military reconnaissance - the radar imaging version of Condor-E. Separated from the launch vehicle at 05:05 UTC. Launch was timed to put the satellite into the same orbit plane as its predecessor, Cosmos 2487 (2013-32A/39194). Reportedly built and launched for an overseas customer - South Africa. The upper stage of the launch vehicle was not catalogued because it made a destructive re-entry above the southern Pacific Ocean about 55 minutes after lift off.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 19, 08:32	6878	0.0002	499	501	94.62	74.75	235

Strela Platform 2014-084B 40354						Re-entered - 2024 Oct 12 Life 3585 days
Modified warhead carrier that provided Condor's final impetus to orbit and then released the satellite.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )
2014 Dec 20, 04:36	6847	0.0046	437	500	93.97	74.74	321

2014-085 Angara A5 + Briz-M Plesetsk Cosmodrome						2014 Dec 23, 05:57
Briz-M rocket stage 2014-085A 40355						in space
Carried on test flight of Angara 5 launch vehicle. A satellite mass simulator remained intentionally attached to the Briz-M stage. The stage issued a satellite separation command at 14:58 UTC to confirm completion of the main mission. The first four orbits listed are estimates based on publicly available data.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Dec 23, 06:11	6561	0.0011	175	190	88.14	64.60	80
2014 Dec 23, 07:30	9011	0.2627	266	4999	141.87	62.60	359
2014 Dec 23, 09:59	24499	0.7215	445	35796	636.02	60.60	0
2014 Dec 23, 15:00	42178	0.0001	35795	35805	1436.78	0.05	180	9°.9 E
2015 Jan 12, 06:16	44001	0.0333	36155	39090	1530.91	0.30	203
2023 Feb 12, 10:12	44001	0.0354	36064	39182	1530.92	7.17	325

2014-086 Soyuz-2.1b Plesetsk Cosmodrome						2014 Dec 25, 03:01
Cosmos 2502 (Lotos-S1 № 1) 2014-086A 40358						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 ( ° )
2014 Dec 25, 16:11	6948	0.0475	240	900	96.06	67.15	92
2014 Dec 27, 19:19	7282	0.0006	900	909	103.08	67.15	237
2014 Dec 31, 13:37	7284	0.0007	901	910	103.11	67.15	263

2014-087 Soyuz-2.1b Baikonur Cosmodrome						2014 Dec 26, 18:55
Resurs-P 2 (Resurs-P №2 ) 2014-087A 40360						Re-entered - 2025 Feb 12 Life 3701 days
Remote sensing, also carrying 'Nucleon' - a package of instruments is intended to study antimatter, dark matter and strange matter through detection and analysis of galactic cosmic rays. Equipped with an AIS (Automatic Information System) receiver to capture positional and movement information from ships at sea. Orbit adjustments ceased at the end of 2017. Under control until the end of 2021 when stabilisation system failed or was switched off and orbit decay accelerated.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Dec 27, 04:07	6686	0.0179	188	428	90.69	97.29	60	11:48
2014 Dec 29, 12:25	6779	0.0105	330	472	92.59	97.29	90	11:49
2014 Dec 31, 14:16	6845	0.0008	461	472	93.93	97.29	78	11:49
2023 Feb 13, 12:39	6824	0.0007	440	451	93.49	97.19	304	11:06

2014-088 CZ 4B Taiyuan Space Centre						2014 Dec 27, 03:22
Yaogan 26 2014-088A 40362						in space
Described as being used for remote sensing for natural resources surveys. Specific tasks include land survey, crop yield assessment, and input to disaster monitoring and prevention plans. Mission is probably military or government photo-reconnaissance.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	Desc Node Local Time
2014 Dec 27, 12:47	6865	0.0007	482	491	94.34	97.44	241	10:29
2015 Jan 3, 03:26	6867	0.0003	487	491	94.39	97.44	211	10:29
2023 Feb 13, 11:10	6873	0.0009	489	501	94.51	97.12	321	08:16

2014-089 Proton-M + Briz-M Baikonur Cosmodrome						2014 Dec 27, 21:37
Astra 2G 2014-089A 40364						in space
Satellite to provide broadcast, VSat and broadband services to Europe, the Middle East and Africa. Launch originally planned for Nov 27 but announced Nov 26 that a gyro aboard the Briz-M had failed on-pad testing so the Proton was rolled back to the assembly area for repairs. Precise launch time - 21:37:49 UTC. Separated from the Briz-M Dec 28 at 06:49:49 UTC. The first four listed orbits are based on data provided by Khrunichev. Expected location - 28°.2 east.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Dec 27, 21:53	6562	0.0010	177	191	88.18	51.56	80
2014 Dec 28, 01:25	9012	0.2627	266	5000	141.89	50.31	358
2014 Dec 28, 04:03	24473	0.7231	398	35793	635.04	49.10	359
2014 Dec 28, 06:37	26304	0.6004	4133	35718	707.59	22.98	0
2014 Dec 29, 16:02	28384	0.4835	8281	35730	793.16	14.24	1
2014 Dec 31, 14:39	31861	0.3215	15239	35726	943.28	7.50	1
2015 Jan 1, 03:54	37809	0.1137	27131	35731	1219.41	2.05	2
2015 Jan 4, 02:53	42082	0.0007	35675	35732	1431.87	0.09	153	19°.8 E
2015 Jan 8, 16:41	42165	0.0001	35785	35789	1436.11	0.09	184	21°.1 E
2015 Apr 23, 22:59	42060	0.0000	35680	35684	1430.75	0.07	23	31°.0 E
2015 May 5, 18:00	42166	0.0001	35782	35793	1436.14	0.05	43	43°.5 E
2015 May 24, 19:08	42216	0.0001	35831	35844	1438.70	0.03	93	42°.1 E
2015 Jun 19, 00:00	42166	0.0005	35768	35807	1436.14	0.05	360	28°.2 E
2023 Feb 12, 13:08	42165	0.0003	35773	35800	1436.09	0.04	43	28°.2 E

2014-090 CZ 3A Xichang Space Centre						2014 Dec 31, 01:02
Fengyun 2G (Fengyun 2-05) 2014-090A 40367						in space
Meteorological imaging and climate monitoring satellite, replacement for Fengyun 2D (2006-053A/29640). Tested at 100° east then moved to its operational location at 105° east where it arrived 2015 Jun 1.
epoch (UTC)	s-m axis ( km )	eccentricity	perigee ( km )	apogee ( km )	period ( min )	incl ( ° )	ω ( ° )	GEO Longitude
2014 Dec 31, 06:46	25140	0.7335	321	37203	661.16	24.55	181
2015 Jan 8, 13:27	42163	0.0003	35770	35800	1436.02	2.27	236	99°.8 E
2015 May 24, 00:03	42115	0.0005	35717	35757	1433.56	1.99	261	100°.0 E
2015 Jun 1, 20:18	42165	0.0006	35763	35811	1436.10	1.97	258	104°.9 E
2018 Apr 9, 17:20	42167	0.0001	35784	35793	1436.21	0.30	194	104°.4 E
2018 Apr 10, 14:17	42277	0.0005	35875	35922	1441.82	0.30	132
2018 Apr 13, 19:12	42125	0.0008	35711	35782	1434.05	0.31	230	99°.2 E
2018 Apr 14, 21:25	42163	0.0002	35775	35794	1435.99	0.31	200	99°.2 E
2023 Feb 13, 10:07	42167	0.0001	35784	35794	1436.23	2.54	284	99°.5 E