2003-028A
BSAT-2c was launched as the lower payload with Optus and Defence C1. under a SYLDA-5 on Ariane 515G.
Satellite is an Orbital Star-1. Uses Star 30BCP motor. Launch mass 1275 kg, 535 kg dry - total of 740 prop.
Star 30C is 630 full 33 empty - 597 prop. This leaves 143 kg of on orbit prop. Star 30E is 667 full 45 empty, 622 prop, leaving 118 kg on orbit prop. Star 30CBP is probably closer to 30E?
box + 2 panels 3.7 x 2.5 x 2.0m with 11.5m span. To be at 110E to provide digital TV broadcasting to Japan.
| BSAT 2c | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2003 Jun 11 | 2238 | Launch by Ariane 5G | CSG ELA3 |
| T+2:22 EAP sep | |||
| T+3:20 Fairing sep | |||
| T+9:45 EPC MECO | |||
| 2247 | T+9:52 EPC sep | 55 x 1972 x 7.46 | |
| 2248 | T+9:59 EPS MES | ||
| 2304 | T+26:52 EPS MECO | ||
| 2306 | T+28:07 Optus sep | ||
| 2309 | T+31:59 Sylda 5 sep | ||
| 2313 | T+35:02 BSAT 2 sep | ||
| T+51:21 end of V161 mission is | |||
| 2003 Jun 12 | 0025? | EPC reentry | |
| 2003 Jun 13 | 639.63 604 x 35821 x 7.00 | ||
| 2003 Jun 16 | 0340? | AKM | |
| 1404.44 34557 x 35772 x 0.33 90.4E dr | |||
| 2003 Jun 19 | 1426.25 35381 x 35805 x 0.13 GEO 113E+2/d | ||
| 2003 Jul 3 | 1436.10 35766 x 35806 x 0.1 GEO 120.6E | ||
| 2003 Jul 15 | OSC on orbit delivery | ||
| 2003 Oct 3 | 1436.16 35771 x 35803 x 0.1 GEO 109.9E | ||
| 2006 Aug 7 | 1436.16 35770 x 35805 x 0.1 GEO 109.9E | ||
| 2010 Apr 29 | 1436.16 35776 x 35799 x 0.0 GEO 109.9E | ||
| 2013 Jul 21 | 1436.12 35774 x 35800 x 0.06 GEO 109.9E | ||
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