2007-025A
Mass 300 kg. Built by IAI, for Israeli Defense Forces imaging.
| Ofeq 7 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2007 Jun 10 | 2340 | Launch by Shavit | PAL |
| Stage 1 MECO at T+0:52 | |||
| 2341? | Stage 1 sep | ||
| Stage 2 MECO at T+1:44, | |||
| 2342? | Stage 2 sep, 110 km | ||
| 2347? | Fairing (2 pieces) sep, 250 km | ||
| 2347? | Main equipment compartment sep | ||
| 2349? | Stage 3 92s burn over W Med. | ||
| 2350? | Stage 3 sep | 93.34 299 x 576 x 141.75 | |
| 2007 Jun 11 | 0028? | Ofeq apogee burn | 93.75 340 x 576 x 141.75 |
2001-045A
Another Globus military comms satellite was launched in Oct 2001.
| Raduga-1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2001 Oct 6 | 1645:00 | Launch by Proton | KB LC81/24 |
| Stage 2 sep | |||
| 1654 | Stage 3 MECO | ||
| 1654:41 | Stage 3 sep | ||
| 1655 | Adapter sep | ||
| 1758:28 | DM2 MES-1 | ||
| 1805:29 | DM2 MECO-1 | ||
| 633.87 223 x 35906 x 48.75 | |||
| 2316:44 | DM2 MES-2 | ||
| 2319:55 | DM2 MECO-2 | ||
| 2320:03 | DM2 sep | ||
| 2001 Oct 7 | 1328.57 32309 x 35000 x 1.5 | ||
| 2001 Oct 20 | 1435.99 35776 x 35792 x 1.5 GEO 84.7E | ||
| 2001 Dec 4 | 1436.11 35777 x 35796 x 1.4 GEO 85.3E | ||
| 2003 Nov 13 | 1436.17 35780 x 35795 x 0.5 GEO 85.2E | ||
| 2003 Dec | Relocate to 70E | ||
| 2003 Dec 29 | 1436.14 35783 x 35791 x 0.5 GEO 69.6E | ||
| 2004 Feb 28 | 1436.01 35777 x 35792 x 0.7 GEO 70.2E | ||
| 2005 Jun 15 | 1436.10 35774 x 35799 x 1.9 GEO 69.7E | ||
| 2005 Oct 5 | 1436.10 35772 x 35801 x 2.2 GEO 70.0E | ||
| 2005 Oct 11 | Orbit raise | 1441.94 35787 x 36014 x 2.2 | |
| 2005 Nov 13 | Relocate at 26E | ||
| 2005 Nov 20 | 1436.12 35769 x 35804 x 2.3 GEO 26.7E | ||
| 2006 Feb 15 | 1435.90 35775 x 35790 x 2.6 GEO 27.5E | ||
1972-016A
The first GAMBIT flight of 1972 was launched on Mar 17 from Vandenberg. The mission lasted 25 days (24 days photographic). Launch vehicle for this flight was the Titan 23B Agena D according to Martin Marietta documents; this is probably just a new designation for the IIIB rather than a new variant of the vehicle. The vehicle was deorbited over Eniwetok as part of the VAST 4 reentry-survival experiment.
| KH-8 OM 34 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1972 Mar 17 | 1700 | Launch by Titan 23B Agena D | V SLC4W |
| 1702 | Titan stage 1 sep | ||
| 1705 | Titan stage 2 sep | ||
| 1705 | Agena burn | ||
| 1710? | Agena MECO | ||
| 1930 | 89.95 128 x 415 x 111.0 | ||
| 1972 Mar 19 | 0557 | 89.76 130 x 393 x 111.0 | |
| Orbit raise | |||
| 2224 | 89.84 130 x 402 x 111.0 | ||
| Orbit raise | |||
| 1972 Mar 21 | 2046 | 89.98 133 x 413 x 111.0 | |
| 1972 Mar 26 | 0534 | 89.60 132 x 376 x 111.0 | |
| Orbit raise | |||
| 2329 | 89.94 141 x 400 x 111.0 | ||
| 1972 Mar 29 | 1123 | 89.70 139 x 379 x 111.0 | |
| Orbit raise | |||
| 1972 Mar 30 | 0221 | 89.88 140 x 396 x 111.0 | |
| 2050? | SRV-1 deorbit opportunity rev 212 | ||
| 2057? | Entry | ||
| 2125? | SRV-1 recovered | ||
| 1972 Mar 31 | 0519 | 89.77 140 x 385 x 111.0 | |
| Orbit raise | |||
| 1972 Mar 31 | 2146 | 89.85 140 x 393 x 111.0 | |
| 1972 Apr 3 | 0508 | 89.63 138 x 374 x 110.9 | |
| Orbit raise | |||
| 1972 Apr 4 | 1403 | 89.88 143 x 393 x 110.9 | |
| 1972 Apr 5 | 2300 | 89.77 143 x 382 x 110.9 | |
| Orbit raise | |||
| 1972 Apr 6 | 2256 | 89.85 142 x 391 x 110.95 | |
| 1972 Apr 8 | 0622 | 89.75 142 x 381 x 110.9 | |
| Orbit raise | |||
| 1972 Apr 8 | 2250 | 89.88 142 x 394 x 110.9 | |
| 1972 Apr 9 | 1349 | 89.83 142 x 389 x 110.9 | |
| 1972 Apr 10 | 2315? | SRV-2 deorbit opportunity | |
| 2322? | Entry | ||
| 2350? | SRV-2 recovery | ||
| 1972 Apr 11 | Reentered after 25 days | ||
| 0044? | Agena deorbit over Alaska, perhaps -120 to -150 m/s ? | ||
| 0057 | VAST 4 controlled reentry at Eniwetok | ||
