1999-051A
Mass 726 kg. Built by LM/Sunnyvale using LM900 bus. Ikonos had 1-m resolution at 13 km swath. Launched to 10:30am descending node SSO. Ikonos was the first of the high res commercial imaging satellites to reach orbit and operate.
A piece of debris separated on 2001 Mar 19 and reentered rapidly.
OAM mass 650f?; Orbus 21 10600 f 865 em so m1/m2 = 11976 / 2241
| Ikonos | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1999 Sep 24 | 1821:08 | Launch by Athena 2 LM-7 | V SLC6 |
| T+1:24 St 1 burnout | |||
| T+1:25 St 2 burn 18 km | -6300 x 20 ? | ||
| T+2:53 St 2 burn out | -5600 x 180 ? | ||
| T+4:27 Fairing | -5600 x 180 ? | ||
| T+4:32 St 2 sep | |||
| 1825:40 | T+4:32 St 3 burn at 179 km | ||
| 1828:11 | T+7:03 St 3 burnout | ||
| 1828:12 | T+7:04 St 3 sep 90.92 207 x 431 x 98.2 (B) | ||
| 1828:17 | T+7:09 St 4 burn 162s | ||
| 1830:59 | T+9:51 St 4 MECO | 93.69 220 x 689 x 98.2 (est) | |
| 1912:35 | T+51:27 St 4 burn 2 386s | ||
| 1919:01 | T+57:53 St 4 MECO-2 | ||
| 1919:15 | T+58:07 St 4 sep | 98.36 678 x 682 x 98.1 | |
| 1924 | T+1:03:08 St 4 avoidance | ||
| 1928 | T+1:07:26 St 4 MECO-3 | 92.24 137 x 630 x 97.7 (C) | |
| 98.36 678 x 682 x 98.1 | |||
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