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JCSAT-RA

JCSAT-RA, previously known as JCSAT-12,[2] is a Japanese geostationary communications satellite, which is operated by SKY Perfect JSAT Group.

JCSAT-RA
Mission typeCommunication
OperatorSKY Perfect JSAT Group
COSPAR ID2009-044A
SATCAT no.35755
Mission duration15 years
Spacecraft properties
BusA2100AXS
ManufacturerLockheed Martin
Launch mass4,000 kilograms (8,800 lb)
Start of mission
Launch date21 August 2009, 22:09 (2009-08-21UTC22:09Z) UTC
RocketAriane 5ECA
Launch siteKourou ELA-3
ContractorArianespace
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Perigee altitude35,787 kilometres (22,237 mi)[1]
Apogee altitude35,798 kilometres (22,244 mi)[1]
Inclination0.04 degrees[1]
Period1436.11 minutes[1]
Epoch24 January 2015, 13:19:57 UTC[1]
 

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. ^ a b c d e "JCSAT 12 Satellite details 2009-044A NORAD 35755". N2YO. 24 January 2015. Retrieved 25 January 2015.
  2. ^ a b Krebs, Gunter. "JCSat 10, 11, 12 (JCSat 3A, RA)". Gunter's Space Page. Retrieved 31 July 2010.
  3. ^ (PDF). JSAT Corporation. 6 September 2007. Archived from the original (PDF) on 21 July 2011. Retrieved 21 August 2009.
  4. ^ . Satnews Daily. Archived from the original on 5 October 2007. Retrieved 21 August 2009.
  5. ^ "Preparations continue with the JCSAT-12 and Optus D3 payloads for Ariane 5's next launch". Mission Update. Arianespace. 12 August 2009. Retrieved 21 August 2009.

jcsat, previously, known, jcsat, japanese, geostationary, communications, satellite, which, operated, perfect, jsat, group, mission, typecommunicationoperatorsky, perfect, jsat, groupcospar, id2009, 044asatcat, 35755mission, duration15, yearsspacecraft, proper. JCSAT RA previously known as JCSAT 12 2 is a Japanese geostationary communications satellite which is operated by SKY Perfect JSAT Group JCSAT RAMission typeCommunicationOperatorSKY Perfect JSAT GroupCOSPAR ID2009 044ASATCAT no 35755Mission duration15 yearsSpacecraft propertiesBusA2100AXSManufacturerLockheed MartinLaunch mass4 000 kilograms 8 800 lb Start of missionLaunch date21 August 2009 22 09 2009 08 21UTC22 09Z UTCRocketAriane 5ECALaunch siteKourou ELA 3ContractorArianespaceOrbital parametersReference systemGeocentricRegimeGeostationaryPerigee altitude35 787 kilometres 22 237 mi 1 Apogee altitude35 798 kilometres 22 244 mi 1 Inclination0 04 degrees 1 Period1436 11 minutes 1 Epoch24 January 2015 13 19 57 UTC 1 JSAT JCSAT 11JCSAT 13 Details EditIt 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 Edit Spaceflight portal2009 in spaceflightReferences Edit a b c d e JCSAT 12 Satellite details 2009 044A NORAD 35755 N2YO 24 January 2015 Retrieved 25 January 2015 a b 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 6 September 2007 Archived from the original PDF on 21 July 2011 Retrieved 21 August 2009 Arianespace amp JSAT Culminate Contract For JCSAT 12 Satnews Daily Archived from the original on 5 October 2007 Retrieved 21 August 2009 Preparations continue with the JCSAT 12 and Optus D3 payloads for Ariane 5 s next launch Mission Update Arianespace 12 August 2009 Retrieved 21 August 2009 Retrieved from https en wikipedia org w index php title JCSAT RA amp oldid 1105512528, wikipedia, wiki, book, books, library,

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