2008-004A
Progress M No 363. Mass 7283 kg.
| PM63 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2008 Feb 5 | 1302:57 | Launch by Soyuz-U | KB LC1 |
| T+1:58 Strapons sep | |||
| T+2:42 GO sep | |||
| T+4:45 Blok A MECO | |||
| T+4:47 Blok A sep | |||
| T+4:57 KhO sep | |||
| T+8:45 Blok I MECO | |||
| 1311:46 | T+8:49 Blok I sep | ||
| 2008 Feb 5 | |||
| 1650:18 | DV1 62.2s 25.3m/s SKD | ||
| 1735:40 | DV2 21.7s 8.5m/s SKD | ||
| 2008 Feb 6 | 1406:31 | DV3 1.5m/s SKD | |
| 2008 Feb 7 | |||
| 1430:13 | Docking with Pirs | ||
| 2008 Apr 7 | 0849 | Undocked | |
| 1150 | Deorbit | ||
2007-058A
Globus-1M comms satellite, 17F15M.
Launched by Proton-K No. 53526 with Briz-M No. 88526. Given the cover name Raduga-1M (although the KV press center called it Kosmos-2434, this name was not used in later official statements).
| Raduga-1M | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2007 Dec 9 | 0015 | Launch by Proton-M | KB LC81 |
| T+2:06 St 1 sep | |||
| T+3:03 GO sep | |||
| T+5:30 St 2 sep | |||
| 0024 | T+9:34 St 3 MECO | ||
| T+9:44 Stage 3 sep | |||
| 0026 | T+11:19 ?Briz MES-1 | ||
| 0033 | T+18:55? MECO-1 | 173 x 173 x 51.49 | |
| 0123? | T+1:08? MES-2 | ||
| 0140? | T+1:25? MECO-2 | 273 x 4991 x 48.8 | |
| 0345? | T+3:30? MES-3 | ||
| 0356? | T+3:41? MECO-3 | ||
| 0357? | T+3:42? DTB sep | 316 x 17659 x 49.5 | |
| 0358? | T+3:43? MES-4 | ||
| 0403? | T+3:48? MECO-4 | 400 x 35815 x 49.1 | |
| 415 x 35534 x 46.49 | |||
| 0907? | T+8:52? MES-5 | ||
| 0915? | T+9:00? MECO-5 | ||
| 0917 | T+9:02 Briz-M sep | 1378.91 33620 x 35699 x 0.1 | |
| 2007 Dec 18 | 1434.87 35572 x 35952 x 0.1 GEO 79.3E+0.3E/d | ||
| 2008 Jan 14 | 1436.10 35775 x 35797 x 0.1 GEO 70.0E | ||
| 2008 Mar 10 | 1436.08 35780 x 35792 x 0.0 GEO 70.0 | ||
2005-049A
1385 kg dry 3081 kg launch (Arianespace PK).
1690 kg prop; 536 kg left by Dec 26.
2.0 x 1.7 x 2.8m with 15.4m span. Ku/C-band satellite for 83E.
Built at ISAC/Bangalore; Launch by Ariane 5. Insat 4A was on an 1194H adapter, with an ACY2624-M extension on top of the Sylda 5E. The medium fairing was used.
Insat 4A was colocated at 83E with Insat 2E and 3B.
| Insat | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2005 Dec 21 | 2233:00? | Launch by Ariane 5GS | |
| T+2:20 EAP sep | |||
| T+3:22 Fairing sep | |||
| T+9:41 EPC MECO | |||
| 2242:47 | T+9:47 EPC sep | 43.5 x 1701.8 x 6.5 | |
| 2242:54 | T+9:54 EPS burn | ||
| 2259:48 | T+26:48 EPS MECO | ||
| 2302:05 | T+29:05 Insat 4A sep | ||
| 2305:09 | T+32:09 Sylda 5 sep | ||
| 2309:32 | T+36:32 MSG-2 sep | ||
| 2005 Dec 21 | 639.38 603 x 35809 x 3.7 | ||
| 2005 Dec 22 | 0015? | EPC reentry | |
| 2005 Dec 22 | 640.57 620 x 35853 x 3.9 | ||
| 2005 Dec 23 | 0054 | LAM-1 1:25:00 | 916.43 13754 x 35995 x 0.9 |
| 2005 Dec 23 | 916.43 13754 x 35995 x 0.9 | ||
| 2005 Dec 24 | 0754 | LAM-2 42:00 | 1333.00 31479 x 36008 x 0.2 |
| 2005 Dec 26 | 0430 | LAM-3 5:45 to 1434 min | |
| Solar arrays deployed | |||
| 2005 Dec 31 | 1436.00 35776 x 35793 x 0.1 GEO 81.5E | ||
| 2006 Feb 16 | 1436.11 35762 x 35811 x 0.1 GEO 82.9E | ||
2007-064A
Flight 27P, spacecraft 11F615A55 No 362. Launch mass 7136 kg including 2430 kg of cargo.
| PM62 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2007 Dec 23 | 0712:41 | Launch | |
| T+1:58 Strapons sep | |||
| T+2:42 GO sep | |||
| T+4:45 Blok A MECO | |||
| T+4:47 Blok A sep | |||
| T+4:57 KhO sep | |||
| 0721:26 | T+8:45 Blok I MECO | ||
| 0721:30 | T+8:49 Blok I sep | ||
| 1102:07 | SKD burn 41s 16.8m/s | ||
| 1144:52 | SKD burn 10.6s 4.4m/s | ||
| 2007 Dec 25 | 0756:21 | SKD burn 2.2m/s | |
| 2007 Dec 26 | 0754 | Rendezvous with ISS at 400m | |
| 0758 | Approach from 180m | ||
| 0814:06 | Docked with Pirs | ||
| 2008 Feb 4 | 1031:52 | Undocked | |
| 1035 | Sep-1 15s | ||
| 1339:30 | DV-1 3m/s Plazma-Progress | ||
| 2008 Feb 10 | 1112:59 | DV-2 3m/s | |
| 2008 Feb 11 | 1000:36 | DV-3 3m/s | |
| 2008 Feb 12 | 1022:45 | DV-4 1m/s | |
| 2008 Feb 13 | 0909:33 | 1m/s | |
| 2008 Feb 14 | 0931:09 | 3m/s | |
| 2008 Feb 15 | 0944:00 | Deorbit burn 84.5m/s 140.7s | |
| 0946:21 | Deorbit cutoff | ||
| 1018:36 | Entry | ||
| 1023:36 | Breakup 70 km | ||
| 1029:34 | Debris impact Pacific | ||
2001-002A
Eurasiasat (Turksat 2) was a joint venture between Turk Telecom/Ankara and Aerospatiale. The satellite was registered with the UN by Turkey.
| Eurasiasat 1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2001 Jan 10 | 2209 | Launch by Ariane 44P V137 | CSG ELA2 |
| T+1:11 PAP sep | |||
| T+3:31 St 1 sep | |||
| T+3:33 St 2 TIG | |||
| T+4:26 Fairing | |||
| T+5:43 St 2 sep | |||
| T+5:48 St 3 MES | |||
| 2227 | T+18:54 St 3 MECO | ||
| 2229 | T+20:20 St 3 sep | ||
| T+20:25 St 3 avoidance | |||
| 2001 Jan 11 | 0730 | H10-3 reentered | |
| 2001 Jan 12 | 792.91 8283 x 35715 x 2.9 | ||
| 2001 Jan 14 | 1078.29 21192 x 35716 x 1.0 | ||
| 2001 Jun 5 | 1436.06 35779 x 35792 x 0.0 GEO 42.0E | ||
| 2006 Jul 22 | 1436.08 35778 x 35793 x 0.04 GEO 42.0E | ||
2008-048A
Falcon 1 Flight 4 carried a payload mass simulator nicknamed Ratsat. The hexagonal prism was 1.5m long and had a mass of 165 kg. The simulator was designed to remain attached to the second stage. This launch was the first to successfully reach orbit.
| F4 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2008 Sep 28 | 2315 | Launch by Falcon 1 | Omelek |
| T+2:37 MECO | |||
| T+2:42 St 1 sep | |||
| T+2:45 Kestrel MES | |||
| T+2:53 Jettison nozzle stiffeners | |||
| T+3:15 Fairing sep | |||
| 2324 | T+9:39 SECO | 330 x 650? x 9.0 | |
| Coast 43.5min | |||
| 2008 Sep 29 | 0008 | T+53m Stage 2 restart 6.8s | |
| SECO-2 | 621 x 643 x 9.35 | ||
