JCSAT-RA
| Mission type | Communication | ||||
|---|---|---|---|---|---|
| Operator | SKY Perfect JSAT Group | ||||
| COSPAR ID | 2009-044A | ||||
| SATCAT № | 35755 | ||||
| Mission duration | 15 years | ||||
| Spacecraft properties | |||||
| Bus | A2100AXS | ||||
| Manufacturer | Lockheed Martin | ||||
| Launch mass | 4,000 kilograms (8,800 lb) | ||||
| Start of mission | |||||
| Launch date | 21 August 2009, 22:09 UTC | ||||
| Rocket | Ariane 5ECA | ||||
| Launch site | Kourou ELA-3 | ||||
| Contractor | Arianespace | ||||
| Orbital parameters | |||||
| Reference system | Geocentric | ||||
| Regime | Geostationary | ||||
| Perigee | 35,787 kilometres (22,237 mi)[1] | ||||
| Apogee | 35,798 kilometres (22,244 mi)[1] | ||||
| Inclination | 0.04 degrees[1] | ||||
| Period | 1436.11 minutes[1] | ||||
| Epoch | 24 January 2015, 13:19:57 UTC[1] | ||||
| |||||
JCSAT-RA, previously known as JCSAT-12,[2] is a Japanese geostationary communications satellite, which is operated by SKY Perfect JSAT Group.
Details
It was ordered to replace the JCSAT-11 satellite which was lost in a launch failure on a Proton-M/Briz-M rocket in 2007, and is currently used as an on-orbit spare satellite; a role in which it replaced the older JCSAT-R spacecraft, providing a reserve for if one of the company's other satellites fails. It is a 4,000-kilogram (8,800 lb) satellite, which was constructed by Lockheed Martin based on the A2100AX satellite bus, with the same configuration as JCSAT-10 and JCSAT-11.[2] The contract to build JCSAT-12 was awarded on 6 September 2007, the day after JCSAT-11 failed to reach orbit.[3]
It was launched, along with the Australian Optus D3 satellite, by Arianespace.[4] An Ariane 5ECA rocket was used for the launch, which occurred from ELA-3 at the Guiana Space Centre in Kourou, French Guiana. The launch took place at 22:09 GMT on 21 August 2009, at the start of a 60-minute launch window.
JCSAT-12 separated from its carrier rocket into a geosynchronous transfer orbit, from which raise itself to geostationary orbit using a LEROS-1C apogee motor. It has a design life of fifteen years, and carries forty two transponders; twelve G/H band, and thirty J band (US IEEE C and Ku bands respectively).[5]
See also
References
- 1 2 3 4 5 "JCSAT 12 Satellite details 2009-044A NORAD 35755". N2YO. 24 January 2015. Retrieved 25 January 2015.
- 1 2 Krebs, Gunter. "JCSat 10, 11, 12 (JCSat 3A, RA)". Gunter's Space Page. Retrieved 31 July 2010.
- ↑ "Order of the Replacement Satellite of JCSAT-11 Backup Satellite Following Launch Failure" (PDF). JSAT Corporation. 2007-09-06. Retrieved 2009-08-21.
- ↑ "Arianespace & JSAT Culminate Contract For JCSAT-12". Satnews Daily. Retrieved 2009-08-21.
- ↑ "Preparations continue with the JCSAT-12 and Optus D3 payloads for Ariane 5's next launch". Mission Update. Arianespace. 2009-08-12. Retrieved 2009-08-21.