2015-061A
Tianhui yihao 03 xing (Tianhui-1C) was launched in 2015 at the same time of day.
| TH1C | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2015 Oct 26 | 0710 | Launch by CZ2D | JQ SLS2 (LC43 Pad 603) |
| T+2:36 St 1 MECO | |||
| T+2:36 St 1 sep | |||
| St 2 burn | |||
| 0712 | T+3:06 Fairing sep | ||
| 0715 | T+5:34 Stage 2 MECO | ||
| 0720 | T+10:26 Stage 2 VECO | ||
| 0721 | T+11:11 Stage 2 sep | 490 x 500 x 97.4 | |
| Stage 2 deorbit | |||
2015-078A
DAMPE, the Dark Matter Particle Explorer, was named Wukong before launch. Will find high energy gamma rays (5 GeV-10 TeV), electrons (5 GeV-10 TeV) and cosmic rays (0.1-100 TeV); look for indirect evidence of dark matter decays. Angular resolution is 0.1 deg at 100 GeV.
1900 kg satellite of which 1400 kg is payload. Box + 2 panels Launched to 500 km SSO at 0632 LTDN.
| DAMPE | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2015 Dec 17 | 0012:04 | Launch by CZ-2D | JQ |
| 0018? | St 2 MECO | ||
| 0020 | St 2 VECO | ||
| 0021? | St 2 sep | 94.54 487 x 504 x 97.3 | |
| 0025? | St 2 deorbit | ||
| 0100? | St 2 reentry | ||
2013-054A
Spacecraft No. 710. Crew Oleg Kotov, Sergey Ryazinskiy and Michael Hopkins.
| TMA10M | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2013 Sep 25 | 2058:50 | Launch by Soyuz-FG E15000-46 | KB LC1 |
| T+1:53 SAS sep | |||
| T+1:58 Blok-BVGD sep, 45 km | |||
| T+2:37 GO sep | |||
| T+4:47 Blok A sep | |||
| T+4:57 KhO sep | |||
| 2107:35 | T+8:45 Blok-I MECO | ||
| 2107:38 | T+8:48 Blok-I sep | ||
| 2142:04 | DV1 84.2s 34.0m/s | ||
| 2226:22 | DV2 57.9s 23.4m/s | 304 x 325 x 51.6 | |
| 2323:55 | DV3 22.3s 8.7m/s | ||
| 2013 Sep 26 | |||
| 0004:10 | DV4 29.2s 11.6m/s | 335 x 356 x 51.6 | |
| 0210 | DV4 7.7 | ||
| 0218 | DV5 | ||
| 0221 | DV6, 600m range | ||
| 0223 | Flyaround begins | ||
| 0225 | 300m | ||
| 0234 | Stationkeeping | ||
| 0235 | Final approach, 190m | ||
| 0237 | Range 95 m | ||
| 0242 | Range 25m | ||
| 0245:22 | Docking with Poisk 5h46m | ||
| 0423 | First HO | ||
| 0434 | HO to ISS | ||
| 2014 Mar 10 | |||
| 2055 | HC to ISS | ||
| 2014 Mar 11 | 0002:32 | Undocking from Poisk | |
| 0230:20 | Deorbit burn 4:50 128m/s | ||
| 0235:01 | DO CO | ||
| 0258:05 | Modules sep | ||
| 0301:02 | Entry | ||
| 0323:50 | Landed | ||
2013-017A
For mission 51P, TKG419, flight M-19M returned to the traditional two-day rendezvous. The Kurs-A ASF2 antenna failed to deploy, but the docking proceeded as scheduled despite worries the antenna would foul one of Zvezda's ATV retroreflectors. The final approach time was extended from 11 to 20 minutes following a software patch to work around the antenna issue.
Mass 7288 kg launch (2366 kg cargo with 880 kg KDU prop, 365 kg add.prop, 458 kg water/O2, 1541 kg cargo; 66 kg accounted EVA material) Docking mass 6907 kg. Undocking 5610 kg. Fully unloaded 4394 kg.
| PM19M | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2013 Apr 24 | 1012:16 | Launch by Soyuz-U | KB |
| T+1:58 Strapon sep | |||
| T+2:41 Fairing sep | |||
| T+4:47 Blok A sep | |||
| T+4:57 Blok I burn | |||
| T+8:45 Blok I MECO | |||
| 1021:05 | T+8:49 Blok-I sep | ||
| 1354:23 | DV1 102s 41m/s | ||
| 1445:30 | DV2 67s 27.0m/s | 294 x 360 x 51.6 | |
| 2013 Apr 26 | 1225:27 | Docked with Zvezda | |
| 1530 | HO to ISS | ||
| 2013 Apr 28 | 1003 | 1.5m/s reboost for 33S landing phasing, 222 kg 718s | |
| 2013 May 8 | 0651:00 | 1.47m/s DPO reboost, 33S landing phasing, 14:04, 236kg prop | |
| 2013 May 17 | 0221 | 1.56m/s DPO reboost, 15:22, 227 kg prop | |
| 2013 Jun 11 | |||
| 1358:13 | Undocked Zvezda | ||
| ASF-02 antenna deployed | |||
| 1400:00 | Sep-1 burn, 15s 7.4m/s | ||
| Radar-Progress | |||
| 2013 Jun 14 | 1252:43 | Radar-Progress-8, TCM1 | |
| 2013 Jun 14 | 1429:04 | Radar-Progress-8, TCM2 | 378 x 411 x 51.7 |
| 2013 Jun 16 | 1238:23 | Radar-Progress-8, TCM3 | |
| 2013 Jun 17 | 1142:25 | Radar-Progress-8, TCM4 | |
| 2013 Jun 17 | Radar-Progress-8, TCM5? | ||
| 2013 Jun 18 | 1222:08 | Radar-Progress-8, TCM6 | |
| 2013 Jun 19 | |||
| 1253:31 | Deorbit 178s 101.36m/s | 359 x 419 x 51.6 | |
| 1256:29 | DO CO | 39? x 393 x 51.7 | |
| 1339 | Impact Pacific 46.3S 140.5W | ||
2011-079A
Ziyuan yi hao 02C weixing; improved hi res civil imaging satellite with mass of 2100 kg. The satellite preforms small orbit adjustment every few days.
| ZY1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2011 Dec 22 | 0326:14 | Launch by CZ-4B | TYSC |
| 0339 | T+13m St 3 sep | ||
| 2011 Dec 29 | 100.33 773 x 774 x 98.56 | ||
| 2012 May 17 | 100.32 773 x 774 x 98.56 | ||
| 2013 Jan 6 | 100.32 773 x 774 x 98.52 | ||
| 2014 Mar 16 | 100.32 772 x 774 x 98.47 | ||
2007-056B
Astrium delivers the Eurostar E3000 satellite on orbit to Paradigm, which operates it for the MoD at 53E. Size is 4.5 x 2.9 x 3.7m with 34 m span. Launch mass is 4635 kg. It is the upper satellite in this launch.
V179, L538, ninth of the 30PA Astrium-contracted launchers. Sylda 5A (6.4m high) and long fairing (17m). Skynet is on a PAS1194C adapter, and Star One on a PAS1194S.
Total GTO mass for the flight is 9528 kg, a new record.
| Skynet 5B | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2007 Nov 14 | 2206 | Launch by Ariane 5ECA | CSG ELA3 |
| T+2:19 EAP sep | |||
| T+3:10 Fairing sep | |||
| T+8:58 EPC MECO | |||
| 2215 | T+9:04 EPC sep | -1065 x 168 x 6.21 | |
| 2215 | T+9:08 ESC-A burn | ||
| 2230 | T+24:56 ESC-A MECO | ||
| 2233 | T+27:12 Skynet sep | ||
| 2235 | T+29:23 Sylda 5 sep | ||
| 2239 | T+33:47 Star One C1 sep | ||
| 2251 | T+45:29 end of Ariane mission | ||
| 2007 Nov 16 | 631.18 261 x 35730 x 6.0 | ||
| 2007 Nov 22 | 630.82 267 x 35706 x 6.0 | ||
| 2007 Nov 24 | 1432.69 35572 x 35867 x 0.1 GEO 3.6E+0.8E/d | ||
| 2007 Nov 27 | 1432.83 35669 x 35775 x 0.1 GEO 6.0E+0.8E/d | ||
| 2007 Dec 9 | 1436.08 35782 x 35789 x 0.1 GEO 6.0E | ||
| 2007 Dec 26 | Move out | ||
| 2008 Jan 18 | Move in | 1436.38 35775 x 35809 x 0.1 GEO 52.5E | |
| 2009 Jun 26 | 1436.06 35768 x 35802 x 0.1 GEO 52.8E+0.0/d | ||
| 2013 Apr 1 | 1436.14 35769 x 35804 x 0.1 GEO 52.7E+0.0/d | ||
| 2013 Apr 5 | Begin west drift | ||
| 2013 May 2 | 1438.81 35836 x 35842 x 0.1 GEO 32.7E+0.7W/d | ||
| 2013 May 14 | Move in at 25E | ||
| 2013 May 17 | 1436.35 35769 x 3581 x 0.1 GEO 24.9E | ||
| 2015 Apr 1 | 1436.09 35768 x 35804 x 0.1 GEO 24.3E | ||
2014-078A
6299 kg SS/Loral satellite at 99W. Size 8.4 x 2.2 x 2.4m, span 32.5m. Launched with GSAT 16 and Sylda 5C No 62C.
| DTV14 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2014 Dec 6 | 2040 | Launch by Ariane VA221 | CSG ELA3 |
| 2042 | T+2:13 EAP sep | ||
| 2043 | T+3:12 Fairing sep | ||
| 2048 | T+8:52 EPC MECO | -983 x 161 x 6.32 | |
| 2048 | T+8:58 EPC sep | ||
| 2049 | T+9:13 ESC-A burn | ||
| 2105 | T+25:02 ESC-A MECO | ||
| 2107 | T+27:47 DTV 14 sep | ||
| 2109 | T+29:12 Sylda sep | ||
| 2112 | T+32:13 GSAT-16 sep | ||
| ESC-A depletion | |||
