2016-051A
This was the Quantum Science Experimental Satellite (QUESS). By Jan 2017 the satellite had completed spacecraft bus testing, payload self test and the world-wide integrated link test verifying pointing accuracy and a single quantum channel link.
| QUESS | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2016 Aug 15 | 1740 | Launch by CZ-2D | JQ |
| 1746? | St 2 MECO | ||
| 1748 | St 2 VECO | ||
| 1749? | St 2 sep | 94.54 488 x 504 x 97.4 | |
| 1753? | St 2 deorbit | ||
| 1830? | St 2 reentry | ||
| 2016 Aug 19 | 94.53 487 x 504 x 97.4 | ||
| 2017 Jan | Testing phase complete | ||
2012-001A
The ZY-3 land mapping satellite had a launch mass of 2630 kg.
| ZY3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2012 Jan 9 | 0317:10 | Launch by CZ-4B | |
| T+2:33 Stage 1 MECO | |||
| T+2:34 Stage 1 sep | |||
| T+2:54 Fairing sep | |||
| T+4:37 St 2 MECO | |||
| T+4:47 St 2 VECO | |||
| T+4:48 St 2 sep | |||
| T+4:48 St 3 burn | |||
| 0328? | T+11:18? St 3 MECO | ||
| 0329:35 | T+12:25 ZY 3 sep | ||
| 0331:05 | T+14:05 Vesselsat sep | ||
| 2012 Jan 18 | 94.66 497 x 507 x 97.5 | ||
| 2012 Mar 30 | 94.67 498 x 506 x 97.5 | ||
| 2013 Jul 11 | 94.66 499 x 505 x 97.4 | ||
| 2014 Jun 12 | 94.66 498 x 505 x 97.4 | ||
2009-020A
Thales Alenia Space satellite for Italian Defense Ministry for Italian and NATO defense comms. Launch by Zenit-3SL. Telespazio is investing in Sicral 1B and will sell some of the surplus UHF capacity. Italsat-3000 bus.
Mass 3060 kg (AWST), 3038 kg (Sea Launch). 1680 kg dry. 2.58 x 3.1 x 5.2m launch, 24.4 x 7.8 x 5.2m deployed.
Direzione Generale delle Telecomunicazioni dell'Informatica e delle Tecnologie Avanzate (TELEDIFE) of the Ministero della Difesa
| Sicral 1B | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2009 Apr 20 | 0816 | Launch by Zenit-3SL | |
| T+2:29 St 1 sep 78 km | |||
| T+3:41 Fairing sep 137km | |||
| T+8:29 St 2 sep 232 km | -1949 x 233 | ||
| 0824 | T+8:39 DM burn 1 | ||
| 0833 | T+17:11 MECO-1 225 km | 200 x 14108 x 0 | |
| 0951 | T+1:35:07 DM MES-2 | ||
| 0954 | T+1:38:09 MECO-2 12060 km | 8604 x 35678 x 0 | |
| 1004 | T+1:48:49 DM sep | ||
| T+7:24:49 apogee 1 | 8606 x 35666 x 0 | ||
| 2009 Apr 20 | 796.67 8582 x 35596 x 0.02 | ||
| 2009 May 1 | 1433.53 35692 x 33780 x 0.05 | ||
| 2009 May 8 | 1436.13 35786 x 35787 x 0.1 GEO 11.8E | ||
| 2016 Aug 8 | 1436.12 35772 x 35801 x 0.1 GEO 11.6E | ||
2007-011A
The first medium-orbit Beidou, COMPASS-M1 beidou daohang weixing. The satellite entered a 773.4 minute orbit and remained there. It used PRN code 30.
Part of Zhongguo beidou daohang xitong (China Beidou Navigation System, COMPASS).
| Beidou M1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2007 Apr 13 | 2011 | Launch by CZ-3A | XSC |
| T+2:25? Stage 1 MECO | |||
| T+2:27? Stage 2 MES, Stage 1 sep | |||
| T+3:52? Fairing sep | |||
| T+4:15? St 2 MECO | |||
| T+4:20? St 2 VECO | |||
| 2015? | T+4:21? St 2 sep, St 3 MES-1 | ||
| 2021? | MECO-1 | ||
| 2022? | MES-2? | ||
| 2023? | MECO-2 | ||
| 2023 | Transfer orbit perigee, at eq. | ||
| 2024? | Stage 3 sep | ||
| 2007 Apr 14 | 375.46 197 x 21525 x 55.1 | ||
| 2007 Apr 18? | AKM burn | ||
| 2007 Apr 18 | 773.05 21509 x 21537 x 55.3 | ||
| 2007 May 19 | 773.39 21519 x 21544 x 55.3 | ||
| 2010 Jan 21 | 773.40 21514 x 21549 x 56.1 | ||
| 2013 Aug 28 | 773.37 21517 x 21545 x 56.9 | ||
| 2013 Sep 5 | orbit raise | ||
| 2013 Sep 8 | 811.22 22418 x 22450 x 54.3 | ||
| 2013 Oct 29 | 811.82 22446 x 22451 x 53.8 | ||
| 2014 Jun 10 | 811.96 22450 x 22453 x 53.5 | ||
