2007-031A
Chinasat 6B is a Thales Alenia Space satellite using the Spacebus 4000C2. Launch mass is 4600 kg.
| ZX-6B | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2007 Jul 4 | 1208 | Launch by CZ-3B | Xichang |
| 1234 | T+26m Stage 3 sep | 920.93 233 x 49721 x 24.2 | |
| 2007 Jul 15 | 1441.33 35789 x 35988 x 0.1 GEO 116.8E | ||
| 2007 Jul 18 | 1436.08 35782 x 35790 x 0.05 GEO 115.5E | ||
| 2014 Oct 6 | 1436.07 35773 x 35798 x 0.01 GEO 115.6E | ||
2003-041A
Titan B-36/Centaur TC-20, with an 86' fairing, launched USA 171 on 2003 Sep 9. The azimuth implied a geostationary mission and the satellite is believed to be an Advanced Orion. The UN-registered orbit is typical of geostationary transfer. TC-20 was the last use of the RL10A-3-3A engines.
| USA 171 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2003 Sep 9 | 0429 | Launch by Titan 4B Centaur | |
| T+2:11 St 1 burn | |||
| T+2:26 SRMU sep | |||
| T+3:30 Fairing sep | |||
| T+5:23 Titan St 1 sep | |||
| T+9:19 SECO | |||
| T+9:28 Titan St 2 sep | |||
| 0438 | T+9:49 MES-1 | ||
| 0441 | T+12:00 MECO-1 | 165 x 180? x 28.5? | |
| 0450s | T+21:52 MES-2 | ||
| 0456s | T+27:05 MECO-2 | 630.2 165 x 35778 x 26.7 (UN) | |
| 0457? | MES-2 (based on model TLE) | ||
| 0503? | MECO-2 | 630.2 165 x 35778 x 26.7 (UN) | |
| 1008s | T+5:39:00? MES-3 | ||
| 1010s | T+5:41:00? MECO-3 | ||
| 1018s | T+5:49 TC-20 sep | ||
| 2008 Aug 11 | 1436.12 35589 x 35984 x 3.2 GEO 95.4E | ||
| 2009 Jul 2 | 1436.12 35626 x 35947 x 3.5 GEO 95.5E | ||
| 2011 Aug 12 | 1435.98 35579 x 35989 x 5.0 GEO 90.0E | ||
