1995-011B
The GMS-5 (Himawari-5) satellite was launched on 1995 Mar 17 on the third H-II flight. This flight used extra SSB (Solid Sub Boosters) in addition to the SRBs.
| GMS 5 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1995 Mar 18 | 0801 | Launch by H-II | TNSC |
| T+1:16 SSB burnout 25 km 1.3 km/s | |||
| T+1:30 SSB sep 36 km 1.6 km/s | |||
| T+1:34 SRB burnout | |||
| T+1:37 SRB sep 42 km 1.6 km/s | |||
| T+3:39 Upper fairing sep 128 km 2.8 km/s | |||
| T+5:47 MECO | |||
| T+5:56 Stage 1 sep 222 km 5.3 km/s | |||
| T+6:02 Stage 2 SES-1 | -4400 x 250 ? | ||
| 0813 | T+12:20 SECO-1 | ||
| 0814 | T+13:16 SFU separation | ||
| 0817 | T+16:11 Lower fairing sep | ||
| 0826 | T+25:03 SES-2 | ||
| 0828 | T+27:02 SECO-2 | ||
| 0828 | T+27:52 Stage 2 sep from GMS | ||
| 647.17 346 x 36465 x 25.1 | |||
| 1995 Mar 19 | 0056 | Star 27 burn | |
| 0110 | Star 27 sep | ||
| 1419.06 35483 x 36321 x 1.1 GEO 151.7E+4.3E | |||
| 1995 Apr 1 | 1434.74 35730 x 35789 x 1.1 GEO 159.6E+0.3E | ||
| 1995 Apr 14 | 1436.08 35783 x 35789 x 1.0 GEO 159.7E | ||
| 1995 Jun 5 | 1436.11 35784 x 35789 x 0.9 GEO 159.7E | ||
| 1995 Jun | Move to 140E | ||
| 1995 Jun 13 | Begin data | ||
| 1995 Jun 26 | 1436.10 35779 x 35793 x 0.9 GEO 140.1E | ||
| 1996 Oct 26 | 1436.15 35784 x 35790 x 0.4 GEO 140.0E | ||
| 1999 Oct 6 | 1436.26 35427 x 36151 x 0.4 GEO 140.1E | ||
| 2001 Jul | S Hemisphere coverage reduced | ||
| 2005 May 5 | 1436.20 35780 x 35796 x 3.8 GEO 140.1E | ||
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