1996-053A
The second Inmarsat III was launched in Sep 1996 by Proton from Baykonur. This Lockheed Martin Telecommunications Series 4000 satellite did not carry an apogee motor. It is the Atlantic Ocean Region East satellite. The satellite will replaced AOR E satellite Inmarsat II F2 at 15.5W. The launch was part of a contract between Inmarsat and the KB Salyut (by the time of launch, part of Krunichev). Launch mass was 1130 kg full.
| Inmarsat III G2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1996 Sep 6 | 1737:38 | Launch by Proton | KB |
| 1739 | Stage 2 TIG T+2:04 | ||
| 1739 | Stage 1 sep (T+2:07) | ||
| 1742 | Stage 2 cutoff (T+5:30) | ||
| 1742 | Stage 2 sep (T+5:35) | ||
| 1742 | Fairing sep (T+5:44) | ||
| 1746 | Stage 3 sep (T+9:49) | ||
| 1747 | Interstage sep (T+10:43) | 222 x 235 x 51.6 | |
| 1850 | Blok DM burn 1 (T+1:13:51) | ||
| 1857 | Blok DM MECO (T+1:20:19) | 230? x 36000? x 51.5 | |
| 1996 Sep 7 | 0009 | SOZ burn | |
| 0014 | Blok DM burn 2 (T+6:40:31) | ||
| 1996 Sep 7 | 0032 | Blok-DM sep (T+6:55:32) | |
| 1996 Sep 7 | 1461.43 36250 x 36312 x 2.6 GEO 79.1E+6.3W | ||
| 1996 Oct 9 | 1437.78 35803 x 35836 x 2.7 GEO 14.6W+0.4W | ||
| 1996 Oct 10 | 1438.05 35803 x 35846 x 2.7 GEO 15.0W+0.5W | ||
| 1996 Dec 21 | 1436.12 35766 x 35807 x 2.5 GEO 15.6W | ||
| 1998 Mar 24 | 1436.09 35763 x 35809 x 1.6 GEO 15.5W | ||
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