2003-059A
IAI MBT Div. to build Amos-2. Spacecom Ltd./Tel Aviv is service provider for Amos-2; the satellite was delivered on orbit by IAI. Mass 1350 kg full (or 1374 kg), 646 kg dry, size 2.7 x 2.1 x 2.4m span 11.0m. It will backup Amos 1 at 4W and include service to the eastern US. Launch by Starsem Soyuz-Fregat in Dec 2003.
Followon AMOS HP with 20 Ku-band transponders and 2600 kg mass?
| Amos 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2003 Dec 27 | 2130:00s | Launch by Soyuz-FG/Fregat ST12 | KB PL31/6 |
| T+1:58 BVGD sep | |||
| T+4:13 Fairing sep | |||
| T+4:48 Blok A sep | |||
| T+4:58 KhO sep | |||
| T+8:45 Blok I MECO | |||
| 2138:48 | T+8:48 Blok I sep | 58 x 190 x 51.8 | |
| 2138:53 | T+8:53 SOZ-1 burn | ||
| 2139:49 | T+9:48.5 MES-1 20.5s | ||
| 2140:09 | T+10:09 MECO-1 EPO | 190? x 190? | |
| 2215? | Blok I reentry | ||
| T+1:09:29 SOZ-2 | |||
| 2240:24 | T+1:10:24 MES-2 ascending node=10.25W 25S 25W, 659s | ||
| 2251:23 | T+1:21:23 MECO-2 intermediate 16N 2E | 250? x 35780 x 49? | |
| 2003 Dec 28 | 0403:34 | T+6:33:34 SOZ-3 burn | |
| 0404:29 | T+6:34:29 MES-3 over 90E 0N, 137s | ||
| 0406:46 | T+6:36:46 MECO-3 | 4407 x 35788 x 23.63 | |
| 0406:47 | T+6:46:47 Fregat sep | 4409 x 35779 x 23.58 | |
| 0446:47 | T+7:16:47 SOZ-4 Fregat depletion | ||
| 0447:02 | T+7:17:02 SOZ cutoff | ||
| 2003 Dec 29 | 714.42 4409 x 35779 x 23.58 | ||
| 2003 Dec 30 | 0317 | ABM-1 46min burn | 19000 x 35800 |
| 2040? | Apogee | ||
| 2003 Dec 31 | 1350 | ABM-2 17min burn | 34000 x 35800 |
| 2004 Jan 5 | 1402.99 34439 x 35832 x 0.3 | ||
| 2004 Jan 12 | On Station | GEO 4W | |
| 2004 Feb 19 | Delivered to Spacecom | ||
| 2006 Aug 1 | 1436.07 35777 x 35794 x 0.1 GEO 4.0W | ||
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