2000-032A
\imps{2.5}{images/00032A}
FY-2B was developed by SARTI/Shanghai for CASC. It carries a 1.2km resolution radiometer. Launch mass is 1380 kg.
In the table below, velocities (supplied by CALT) are Earth-fixed.
FY-2C/D/E will have 5 radiometer channels but are otherwise similar.
| FY-2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2000 Jun 25 | 1150 | Launch by CZ-3 | XSC |
| T+2:00 St 1 sep 55 km, 2.274 km/s | |||
| T+4:13 Fairing 178 km, 5.224 km/s | |||
| T+4:17 St 2 sep 181 km, 5.226 km/s | |||
| 1201 | T+11:43 St 3 MECO-1 299 km, 7.089 km/s | -400? x 300 x 27.4 | |
| T+17:48 St 3 MES-2 243 km, 7.189 km/s | |||
| 1213 | T+23:00 St 3 MECO-2 207 km, 9.804 km/s | ||
| 1213 | T+23:44 St 3 sep, 223 km, 9.797 km/s | 233 x 35820 x 27.4 | |
| 2000 Jun 26 | 0358? | AKM burn | |
| AKM sep | |||
| 2000 Jul 2 | 1438.22 35796 x 35859 x 1.1 | ||
| 2000 Jul 6 | First image | ||
| 2000 Jul 8 | 1436.00 35776 x 35793 x 1.1 GEO 104.4E | ||
| 2001 Jun 9 | 1435.72 35766 x 35792 x 0.3 GEO 103.1E | ||
| 2004 Jan 16 | 1436.11 35781 x 35791 x 0.3 GEO 104.7E | ||
| 2004 Oct | Move to 124E | ||
| 2004 Dec 1 | 1436.266 35788 x 35791 x 0.08 123.22E | ||
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