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==References==
==References==
{{reflist}}
{{reflist}}

==External Links==
*[http://i-m.ch/satellite-services/satellite-coverage/thaicom-5-at-78-5e/ International Media Switzerland] Official provider's site


==Notes==
==Notes==

Revision as of 10:52, 12 February 2014

Template:No epoch

Thaicom 5
Mission typeCommunication
OperatorShin Satellite
Thaicom
COSPAR ID2006-020B Edit this at Wikidata
SATCAT no.29163Edit this on Wikidata
Mission duration12 years (planned)
Spacecraft properties
BusSpacebus 3000A
ManufacturerAlcatel Alenia Space
Launch mass2,800 kilograms (6,200 lb)
Start of mission
Launch date27 May 2006, 21:09 (2006-05-27UTC21:09Z) UTC
RocketAriane 5ECA
Launch siteKourou ELA-3
ContractorArianespace
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Longitude78.5° East
Perigee altitude35,777 kilometres (22,231 mi)
Apogee altitude35,796 kilometres (22,243 mi)
Inclination0 degrees
Period24 hours
Transponders
Band25 C band
14 Ku band

Thaicom 5 is a Thai geostationary communications satellite which is operated by Thaicom, and previously Shin Satellite. It is used to provide communications services to Asia, Africa, Europe and Australia.[1]

Overview

Thaicom 5 was constructed by Alcatel Alenia Space, and is based on the Spacebus 3000A satellite bus, with a configuration identical to the Thaicom 3 satellite which it replaced. It was originally ordered as Thaicom 4, but sold to Agrani as Agrani 2 before completion. It was completed in 1997, and stored until June 2005 when it was cancelled and sold back to Shin Satellite as Thaicom 5. It is equipped with 25 G/H band (IEEE C band) and 14 J band (IEEE Ku band) transponders, and at launch it had a mass of 2,800 kilograms (6,200 lb), with an expected operational lifespan of 12 years.[2][3]

Launch

The satellite was launched on an Ariane 5ECA carrier rocket, contracted by Arianespace, flying from ELA-3 at the Guiana Space Centre. The launch occurred at 21:09 GMT on 27 May 2006, and placed Thaicom 5, along with the Mexican Satmex 6 spacecraft, into geosynchronous transfer orbit.[4] At the time, this was the heaviest dual-satellite payload ever launched into geosynchronous transfer orbit,[5] however this record has since been broken.

Following launch, Thaicom 5 raised itself into geostationary orbit using an S400 engine, with insertion occurring on 3 June 2006.[6] It underwent on-orbit testing, and was positioned at a longitude of 78.5° East for operational service, where it replaced the failing Thaicom 3 satellite.[1] On 2 October 2006, after Thaicom 5 had become operational, Thaicom 3 was moved to a graveyard orbit.

See also

References

  1. ^ a b "Thaicom 5". Satellites. Thaicom Public Company Limited. Retrieved 2013-04-09.
  2. ^ "UCS Satellite Database". Union of Concerned Scientists. 2009-07-01. Retrieved 2009-08-08.
  3. ^ Krebs, Gunter. "Thaicom 3, 5". Gunter's Space Page. Retrieved 2009-08-08.
  4. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 2009-08-08.
  5. ^ Launch Webcast. Arianespace. 2006-05-27.
  6. ^ McDowell, Jonathan. "Index". Geostationary Orbit Catalog. Jonathan's Space Page. Retrieved 2009-08-08.

Notes

  • Truevisions is offered through thaicom satellite via c band and ku band signals.
  • Recently with the new nds version 4 update 17 new hd channels have been added.