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 | ||
2010-047A
Launched with two picosats Zheda Pixing 1A-1, 1A-2: 3.5 kilogram with dimension 150mm x 150mm x 150mm and life span for 3 months
The second stage was deorbited without being cataloged. I assume that a large burn over the equator brought the stage down over the Antarctic on the first orbit; this would require about 300 m/s.
The Yaogan 11 satellite is 4th in the YW-2 optical series.
| YW11 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2010 Sep 22 | 0242:04 Launch by CZ-2D | ||
| 0252? | Stage 2 sep | 623 x 657 x 98.0 | |
| 0252? | ZP-1A sep | ||
| 0258? | Stage 2 deorbit? | -440? x 650 x 98.0 | |
| 0320? | Entry over S Pole? | ||
| 2010 Sep 29 | 97.53 624 x 657 x 98.0 | ||
| 2010 Nov 28 | 97.53 622 x 658 x 98.0 | ||
| 2010 Nov 28 | Orbit raise | 97.65 623 x 668 x 98.0 | |
| 2013 Jun 1 | 97.66 625 x 668 x 97.9 | ||
| 2014 Jun 12 | 97.65 626 x 666 x 97.8 | ||
2013-058A
SS/L1300,elliptical orbit satellite, launch mass 6003 kg.
| Sirius FM6 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2013 Oct 25 | 1808:54 | Launch by Proton-M | KB LC200 |
| 1810:53 | St 1 sep | ||
| 1814:20 | St 2 shutdown | ||
| 1814:21 | St 2 sep | ||
| 1814:23 | St 3 burn | ||
| 1814:39 | GO sep | ||
| 1818:36 | OB sep | -516 x 174 x 51.5 | |
| 1820:40 | MDU1 | ||
| 1825:06 | MECO1 | 173 x 173 x 51.52 | |
| 1916:27 | MDU2 | ||
| 1934:12 | MECO2 | 270 x 4999 x 50.33 | |
| 2137:13 | MDU3 | ||
| 2148:41 | MECO3 | 278.06 327 x 15140 x 49.6 | |
| 2149:31 | DTB sep | ||
| 2150:58 | MDU4 | ||
| 2156:54 | MECO4 | 430 x 35809 x 49.1 | |
| 635.27 414 x 35787 x 49.17 | |||
| 2013 Oct 26 | 0300:58 | MDU5 | |
| 0307:10 | MECO5 | 4097 x 35790 x 23.15 | |
| 0320:14 | Sirius sep | 708.44 4074 x 35818 x 23.16 | |
| 0525:34 | SOZ7 | ||
| 0633:34 | SOZ8 | ||
| 2013 Oct 27 | 1430? | LAM1 | 849.20 10837 x 35816 x 11.5 |
| 2013 Oct 29 | 0900? | LAM2 | 1085.71 21418 x 35809 x 4.3 |
| 2013 Oct 31 | 1512? | LAM3 | 1395.95 34203 x 35790 x 0.4 |
| 2013 Nov 1 | 1200? | LAM4 1433.76 35691 x 35790 x 0.1 GEO 122.4W+0.5E/d | |
| 2013 Nov 7 | 1436.13 35783 x 35790 x 0.1 GEO 120.5W | ||
| 2013 Dec 4 | 1436.10 35775 x 35797 x 0.0 GEO 120.5W | ||
