1999-058A
| Globalstar M031 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1999 Oct 18 | 1332:00 | Launch by Soyuz-Ikar | KB LC1 |
| T+1:54 St 1 sep | |||
| T+2:36 Fairing | |||
| T+4:42 St 2 sep | |||
| 1340 | T+8:42 St 3 sep | 240 x 920 | |
| 1601:31 | T+2:29:51 Ikar burn | ||
| 1607:23 | T+2:35:23 Ikar cutoff | ||
| 1704 | T+3:31 Sep 1-3 | ||
| 1704:04 | Sep 4 | ||
| 1999 Oct 20 | 0145? | Ikar deorbit | |
| 0230? | Reentry over S Indian Ocean? | ||
| 1999 Oct 20 | 103.47 894 x 950 x 52.0 | ||
| 1999 Oct 28 | 113.81 1396 x 1406 x 52.0 | ||
| 1999 Nov 5 | 114.08 1412 x 1414 x 52.0 | ||
| 2010 Sep 6 | 114.08 1412 x 1414 x 52.0 | ||
1997-053A
The 803 satellite was swapped to the 42L launch vehicle. The satellite was built by LMT/East Windsor. Its launch mass is 3455 kg, BOL 2079 kg, dry 1601 kg. Bus is 2.5 x 2.2 x 5.2 m with a 10.8m span. Total power is 6400 W. It will be stationed at 26.5W.
In 1998 it became part of the spinoff company New Skies Satellites NV and was renamed NSS-803. It will be moved to the POR to replace NSS-513 in 2002. It was later renamed NSS-5.
| Intelsat 803 (NSS 5) | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1997 Sep 23 | 2358 | Launch by Ariane 42L | CSG ELA2 |
| 1997 Sep 24 | 0000 | T+2:36 PAL sep | |
| 0001 | T+3:23 Stage 1 sep | ||
| 0002 | T+4:13 Fairing 01 sep | ||
| 0003 | T+5:41 Stage 2 sep | ||
| 0003 | T+5:50 Stage 3 burn | ||
| 0016 | T+18:50 Stage 3 MECO | ||
| 0018 | T+20:46 Stage 3 sep | 633.93 291 x 35841 x 7.0 | |
| 0020 | T+22:00 Stage 3 avoidance | ||
| 1040? | Stage 3 reenter on peri 1 | ||
| 1997 Sep 25 | 0235 | 632.16 248 x 35793 x 7.0 | |
| 1997 Sep 25 | 1300? | LAM-1 | |
| 1997 Sep 25 | 1308 | 647.45 2878 x 33947 x 5.7 | |
| 1997 Sep 27 | 1307 | 1155.03 24408 x 35767 x 0.70 | |
| 1997 Sep 28 | 0822 | 1154.88 24409 x 35760 x 0.70 | |
| 1997 Sep 29 | 1300? | LAM-2 | |
| 1997 Sep 29 | 0337 | 1423.12 35281 x 35783 x 0.28 | |
| 1997 Oct 7 | 0224 | 1436.14 35780 x 35794 x 0.1 GEO 27.5W | |
| 1997 Dec 18 | 1436.17 35773 x 35802 x 0.0 GEO 27.6W | ||
| 1997 Dec 19 | mv out | GEO 27.5W | |
| 1997 Dec 24 | mv in | GEO 21.5W | |
| 1998 Feb 18 | 1436.10 35770 x 35802 x 0.0 GEO 21.6W | ||
| 1998 Nov 14 | GEO 21.4W | ||
| 1998 Nov 30 | To New Skies | ||
| 1999 Oct 15 | 1436.11 35775 x 35798 x 0.0 GEO 21.5W | ||
| 2002 Jul 19 | 1436.09 35772 x 35800 x 0.0 GEO 21.5W | ||
| 2002 Oct | Move to 177W | ||
| 2002 Dec 30 | 1436.08 35776 x 35795 x 0.2 GEO 177.0W | ||
| 2003? | Renamed NSS-5 | ||
| 2005 Apr 10 | 1436.09 35774 x 35798 x 0.1 GEO 177.0W | ||
| 2006 Jul 31 | 1436.09 35774 x 35798 x 0.0 GEO 177.0W | ||
| 2009 Apr 14 | move out from 177W | ||
| 2009 Jun 26 | move in at 57E | ||
| 2009 Jul 17 | 1436.10 35785 x 35787 x 0.05 GEO 57.0E | ||
2010-060A
Mass 1900 kg.
| COSMO 4 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2010 Nov 6 | 0220:03 | Launch by Delta 7420-10 | V SLC2W |
| T+1:04 SRB burnout | |||
| T+1:22 SRB sep | |||
| T+4:24 MECO | |||
| T+4:32 Stage 1 sep | |||
| 0224:40 | T+4:37 SEIG-1 | ||
| T+4:41 Fairing sep | |||
| 0231:28 | T+11:25 SECO-1 | 185 x 645 x 97.8 | |
| 0313:30s | T+53:27 SEIG-2 | ||
| 0313:42s | T+53:39 SECO-2 | ||
| 0318:03s | T+58:00 Stage 2 sep | 620 x 632 x 97.8 | |
| 0336:43 | T+1:16:40 SEIG-3 evasive | ||
| T+1:16:45 SECO-3 | 176 x 628 x 97.9 | ||
| 0346s | T+1:26:40 SEIG-4 Depletion burn | ||
| T+1:26:51 Depletion initiation | |||
| T+1:27:08 SECO-4 | 178 x 617 x 98.3 (s) | ||
