2004-018A
Rocsat-2 was renamed Formosat-2 in Dec 2004. It was an Earth imaging satellite with a secondary science payload for imaging lightning.
Rocsat 2 prime contractor was originally DaimlerChrysler Aerospace but after political problems Matra Marconi Space (later EADS Astrium) got the work. Launch 2003. Mass 764 kg including 50 kg of hydrazine. Size 3?m dia 4?m high. hexagon + panel. First use of Astrosat-500 (Leostar 500XO) bus (Spot 5 derivative).
Initial delivery to 730 km orbit, then boost to operational 891 km orbit.
Launch by Taurus XL/3210 with 92" fairing. Control from NSPO MMC at Hsin-Chu in Taiwan.
| ROCSat-2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2004 May 20 | 1747:03 | Launch by Taurus XL 3210 | V 576E |
| T+1:24 Castor 120 sep | |||
| T+2:43 Orion 50SXL burnout | |||
| T+2:47 Orion 50SXL sep | |||
| T+2:50 Orion 50XL burn | |||
| T+2:55 Fairing | |||
| T+4:06 Orion 50XL burnout | |||
| T+5:10 Orion 50XL sep | |||
| T+11:29 Orion 38 burn | -2836 x 714 x 99 | ||
| 1759 | T+12:42 Orion 38 burnout | 728 x 740 x 99 | |
| 1801 | T+14:37 Orion 38 sep | ||
| 730 x 743 x 99.1 | |||
| T+18:02 CCAM burn complete | |||
| T+40:32 RCS depletion | |||
| 2004 May 20 | 99.44 720 x 742 x 99.11 | ||
| 2004 May 23 | 99.50 725 x 743 x 99.10 | ||
| 2004 May 24 | 99.71 734 x 755 x 99.11 | ||
| 2004 May 25 | 100.14 763 x 766 x 99.10 | ||
| 2004 May 27 | 101.11 809 x 812 x 99.1 | ||
| 2004 May 28 | 101.54 829 x 833 x 99.1 | ||
| 2004 Jun 2 | 102.79 890 x 892 x 99.1 | ||
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