2014-090A
fengyun erhao 08 xing; also called FY-2G after launch.
| FY2G | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2014 Dec 31 | 0102 | Launch by CZ-3A | XSC |
| T+2:00 St 1 sep | |||
| T+4:13 Fairing sep | |||
| T+4:17 St 2 sep | |||
| 0113 | T+11:43 St 3 MECO-1 | -400? x 300 x 27.4 | |
| 0119? | T+17:48 St 3 MES-2 | ||
| 0125? | T+23:00 St 3 MECO-2 | ||
| 0125 | T+23:35 Stage 3 sep | ||
2014-009C
Global Precipitation Measuring Mission, Core Spacecraft.
Rainfall and snowfall measurements to 0.2mm accuracy every 3 hours (cf TRMM in equatorial regions only, 0.7mm accuracy every 24 h). TRMM followon.
407 x 407 x 65 Mass 3850 kg. Box + 2 panels Launch as upper payload on H2A 202-4/4D-LS, H2A No 23. Built at GSFC
| GPM-C | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2014 Feb 27 | 1837 | Launch by H2A | Tanegashima |
| T+1:39 SRB burnout | |||
| T+1:48 SRB jettison, 55 km | |||
| 1841 | T+4:05 PLF jettison, 148 km | ||
| 1843 | T+6:36 MECO | ||
| T+6:44 St 1 sep | |||
| T+6:50 SEIG | |||
| 1852 | T+14:58 SECO | ||
| 1852 | T+15:49 GPM sep | ||
| 1901 | T+24:09 Shindaisat sep | ||
| 1905 | T+28:19 STARS-2 sep | ||
| 1909 | T+32:29 Teikyosat-3 sep | ||
| 1913 | T+36:39 ITF-1 sep | ||
| 1914 | T+37:59 OPUSAT sep | ||
| 1916 | T+39:19 INVADER sep | ||
| 1917 | T+40:39 KSAT-2 sep | ||
| 2014 Feb 28 | 92.49 387 x 405 x 65.0 | ||
| 2014 Mar 26 | 92.43 386 x 401 x 65.0 | ||
| 2014 Mar 28 | Orbit raise | 92.53 388 x 408 x 65.0 | |
| 2014 Apr 4 | Orbit raise | 92.58 392 x 409 x 65.0 | |
| 2014 May 29 | 92.54 391 x 406 x 65.0 | ||
| 2014 Jun 1 | Orbit raise | 92.57 393 x 407 x 65.0 | |
| 2014 Jun 18 | 92.53 391 x 405 x 65.0 | ||
| 2014 Jun 21 | Orbit raise | 92.56 393 x 406 x 65.0 | |
| 2014 Jul 9 | 92.53 392 x 404 x 65.0 | ||
| 2014 Jul 12 | Orbit raise | 92.55 391 x 407 x 650 | |
| 2015 Mar | Prop depleted | ||
| 2015 Apr 8 | End of science operations | ||
| 2015 Apr 15 | Decommissioned | ||
2014-070A
Advanced Satellite with New System Architecture for Observation (Asnaro). Managed by Japan Space Systems-USEF (METI), Tokyo and developed by NEC. After delays to Epsilon, launch was transferred to the Russian Dnepr.
NEC NEXTAR bus.
450 kg full 400 kg dry, by NEC/Tokyo. Box-cyl+2 pan.
Launched to 500 km SSO at 1057 LTDN.
| ANSARO | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2014 Nov 6 | 0735:49 | T=0 | |
| 0735:55 | Launch by Dnepr | Yasniy | |
| 0737:36 | T+1:47 St 2 burn | ||
| 0737:40 | St 1 sep | ||
| 0740:17 | T+4:28 St 2 MECO | ||
| 0740:32 | St 2 VECO | ||
| 0740:32? | St 2 sep | ||
| 0740:35 | T+4:46 St 3 burn | ||
| 0749:38 | T+13:49 GO and Platform A sep | ||
| 0749:42 | T+13:53 ASNARO sep | ||
| 0749:44 | T+13:55 Hodo-1 sep | ||
| 0749:46 | T+13:57 Chubu sep | ||
| 0749:47 | T+13:58 QSAT EOS sep | ||
| 0749:48 | T+13:59 TSUBAME sep | ||
| 2014 Nov 21 | 94.78 506 x 509 x 97.5 | ||
