1997-075A
Japan Satellite Systems' JCSAT 5 (JCSAT 1B) is an HS-601, to be at 150E. Launch by Ariane in Dec 1997. JCSAT 5 was launched atop the Cyclade adapter covering the Equator-S science satellite. Provide communication services for Japan and the Asia-Pacific region.
Mass is 2982 kg launch, 1819 kg BOL, 1308 kg dry. Size is 3.80 x 2.80 x 4.30 m with 26.2 m span.
Info on LAM burns provided by Jun Takei of the JCSAT control center in Yokohama.
In 2005 JCSAT 5/1B had thruster problems which pushed its pointing off-target, and it was replaced by JCSAT 4.
| JCSAT 5 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1997 Dec 2 | 2252 | Launch by Ariane 44P | CSG |
| 2255 | T+3:35 Stage 2 burn | ||
| 2256 | T+4:38 Fairing 01 sep | ||
| 2257 | T+5:49 Stage 3 burn | ||
| 2310 | T+18:51 Stage 3 cutoff | ||
| 2312 | T+20:59 JCSAT 5 sep | ||
| 1997 Dec 4 | 630.68 214 x 35751 x 4.0 | ||
| 1997 Dec 4 | 0114:38 | LAM 1 2279s | |
| 1997 Dec 5 | 0115:14 | LAM 2 2656s | |
| 1997 Dec 7 | 0120:28 | LAM 3 1945s | |
| 1997 Dec 7 | 0252:54 | LAM 4 54s | |
| 1997 Dec 7 | 1431.79 35622 x 35781 x 0.1 GEO 138.3E+1.0E | ||
| 1997 Dec 8 | 0045:25 | LAM 5 86s | |
| 1997 Dec 9 | 1436.86 35756 x 35808 x 0.1 GEO 139.4E | ||
| 1998 Jan 3 | 1436.28 35784 x 35795 x 0.1 GEO 139.4E | ||
| 1998 Jan | At 150E replace JCSAT 4 | ||
| 1998 Jan 21 | mv in | 1436.15 35782 x 35793 x 0.0 GEO 150.0E | |
| 1998 Feb 2 | 1436.12 35784 x 35790 x 0.0 GEO 150.0E | ||
| 1999 Oct 15 | 1436.12 35780 x 35793 x 0.0 GEO 150.0E | ||
| 2005 Jan 17 | Thruster anomaly, off line for a few days | ||
| 2005 Jul | Thruster problem recurs | ||
| 2006 Feb 3 | 1436.12 35783 x 35790 x 0.0 GEO 149.9E | ||
| 2006 Feb 5 | Move out of GEO | ||
| 2006 Mar 1 | Move in at 128E | ||
| 2006 Aug 3 | 1436.18 35784 x 35792 x 0.0 GEO 128.0E | ||
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