2003-026A
Boeing GEM launched Jun 2003 by Boeing for Thuraya/Abu Dhabi, to supplement T-1 at 44E. T-3 to follow.
5177 kg launch, 3200 kg BOL. Size is box + 2 panels 7.6 x 3.2 x 3.4m with 40.4m span. T-2 has longer arrays that T-1 with no solar concentrators.
Planned inclination is 6.3 deg at 44E.
| Thuraya 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2003 Jun 10 | 1355:59.2 | Launch by Zenit-3SL | Odyssey |
| T+2:24 St 2 MES | |||
| T+2:29 St 1 sep | |||
| 1359:44 | T+3:45 Fairing sep | ||
| 1404:31 | T+8:32 St 2 sep | -2155 x 187 x 6.3 | |
| 1404:39 | T+8:40 DM MES-1 | ||
| 1409:57 | T+13:38 DM MECO-1 | 180 x 1390 x 6.3 | |
| 1510:41 | T+1:14:42 DM MES-2 | ||
| 1515:58 | T+1:20:59 DM MECO-2 | ||
| 1535:18 | T+1:40:19 DM sep | 649.54 1177 x 35755 x 6.2 | |
| 2003 Jun 11 | 650.79 1207 x 35788 x 6.3 | ||
| 2003 Jun 12 | LAM-1 | 759.15 6604 x 35772 x 6.3 | |
| 2003 Jun 16 | LAM-2 | 1259.69 28752 x 35764 x 6.3 | |
| 2003 Jun 17 | 0830? | LAM-3 | 1388.62 33920 x 35783 x 6.3 |
| 2003 Jun 19 | LAM-4 | 1436.01 35747 x 35822 x 6.3 GEO 28.7E+0.0E | |
| 2003 Jul 28 | 1436.09 35711 x 35861 x 6.2 GEO 28.8E | ||
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