2011-056A
Orbital Star 2.4E, will replace IS 701 at 180E for French Polynesia, the Pacific Islands and connectivity to Western US. Launch by Zenit-3SLB, with Zenit-2SB No. 5L (the former Zenit-2S No. SL32) and DM-SLB No. 5. Launch mass 3200 kg, dry mass 1440 kg, size 5.5 x 3.3 x 2.7m.
| IS-18 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2011 Oct 5 | 2100:02 | Launch by Zenit-3SLB KB | |
| T+2:29 St 1 sep, 85 km | |||
| T+5:18 GO sep, 214 km | |||
| T+8:31 St 2 sep 337 km | -2414 x 410 x 51.38 | ||
| 2108 | T+8:41 Adapter sep 343 km | -2414 x 411 x 51.38 | |
| 2108:37 | T+8:41 MES-1 237.9s 1093.1m/s | ||
| 2112 | T+12:38 MECO-1, 440 km | 175 x 679 x 51.37 | |
| 2220 | T+1:20:03 MES-2 187 km 318.4s 2369.1m/s | 182 x 692 x 51.41 | |
| 2225 | T+1:25:21 MECO-2 302 km | 192 x 35982 x 49.0 | |
| 2011 Oct 6 | |||
| 0322 | T+6:22:25 MES-3 82.9s 1023.6m/s | 198 x 35832 x 48.9 | |
| 0323 | T+6:23:43 MECO-3 | 5518 x 35786 x 19.0 | |
| 0334:29 | T+6:34:34 DM-SL sep | ||
| 0357:49 | DM-SL depletion 33s | ||
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