Mission type | Communication |
---|---|
Operator | APT Satellite |
COSPAR ID | 2012-013A |
SATCAT no. | 38107 |
Website | www |
Mission duration | 15 years[1] |
Spacecraft properties | |
Bus | Spacebus-4000C2 |
Manufacturer | Thales Alenia Space |
Launch mass | 5,054 kilograms (11,142 lb)[1] |
Start of mission | |
Launch date | 31 March 2012, 10:27 | UTC
Rocket | Chang Zheng 3B/E |
Launch site | Xichang LC-2 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 76.5° East[1] |
Perigee altitude | 35,784 kilometres (22,235 mi) |
Apogee altitude | 35,802 kilometres (22,246 mi) |
Inclination | 0.04 degrees |
Period | 23.93 hours |
Epoch | 19 December 2013, 16:37:15 UTC[2] |
Apstar-7 is a Chinese communications satellite which is operated by APT Satellite as part of the Apstar system. It was launched in 2012 as a replacement for the Apstar 2R satellite launched in 1997.[3]
Apstar-7 was constructed by Thales Alenia Space, and is based on the Spacebus-4000C2 satellite bus. The satellite had a mass at launch of 5,054 kilograms (11,142 lb), and is expected to operate for at least 15 years.[1] It is positioned in geostationary orbit at a longitude of 76.5 degrees East, and carries 56 transponders with an operating power of 8.4 kilowatts;[1] 28 operating in the C band and providing services to Asia, Africa, eastern and central Europe and Australia and the other 28 operating in the Ku band, covering Africa, the Middle East, China, and Taiwan.[4] The satellite's solar arrays generate 11.4 kilowatts of power.
Apstar-7 was launched by a Long March 3B/E carrier rocket, flying from Launch Complex 2 at the Xichang Satellite Launch Centre. Liftoff took place at 10:27 UTC on 31 March 2012, with the rocket placing the satellite into a supersynchronous transfer orbit.[5]