1997-069A
Delta Iridium MS-5 was launched on 1997 Nov 9, placing a further five satellites in orbit. The MS-5 launch returned to using the higher 625 x 642 km parking orbit, since the satellite was given a lighter fuel load, reducing mass to 662 kg.
Iridium SV038 raised its orbit in late November, but only reached the engineering orbit of 765 km instead of the operational orbit of 780 km. Its orbit was finally raised to operational height in Apr 1998.
| Iridium 38 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1997 Nov 9 | 0134:26 | Launch by Delta | V SLC2 |
| 0135 | T+1:04 SRM burnout x 6 | ||
| 0135 | T+1:27 SRM sep | ||
| 0136 | T+2:09 SRM burnout x 3 | ||
| 0136 | T+2:11 SRM sep | ||
| 0138 | T+4:20 MECO | ||
| 0138 | T+4:34 St 2 TIG | ||
| 0138 | T+4:43 Fairing sep | ||
| 0145:39 | T+11:13 SECO1 | 170 x 647 x 86.4 | |
| 0232 | T+58:20 TIG 2 | ||
| 0232 | T+58:36 SECO2 | 639 x 639 x 86.6 | |
| 0236:56 | T+1:02:30 SV1 deploy | ||
| 0246:56 | T+1:12:30 SV2 deploy | ||
| 0251:06 | T+1:16:40 SV3 deploy | ||
| 0256:06 | T+1:21:40 SV4 deploy | ||
| 0259:26 | T+1:25:00 SV5 deploy | ||
| 0320 | T+1:45:50 Delta depletion | 254 x 627 x 83.56 | |
| 0320 | T+1:46:05 SECO3 | ||
| 1997 Nov 9 | 97.38 625 x 641 x 86.6 | ||
| 1997 Nov 12 | 97.40 626 x 642 x 86.6 | ||
| 1997 Nov 15 | 97.42 626 x 643 x 86.6 | ||
| 1997 Nov 20 | 98.82 699 x 705 x 86.5 | ||
| 1997 Nov 22 | 100.03 756 x 762 x 86.5 | ||
| 1997 Nov 23 | 100.22 766 x 770 x 86.4 | ||
| 1997 Nov 28 | 100.23 768 x 770 x 86.4 | ||
| 1998 Jan 6 | 100.24 768 x 771 x 86.4 | ||
| 1998 Jan 7 | 100.17 764 x 768 x 86.4 | ||
| 1998 Feb 4 | 100.19 765 x 769 x 86.4 | ||
| 1998 Apr 5 | 100.20 766 x 769 x 86.4 | ||
| 1998 Apr 25 | 100.39 775 x 778 x 86.4 | ||
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