JCSAT-4A: Difference between revisions

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| name = JCSAT-4A (JCSAT-6)
| name = JCSAT-4A (JCSAT-6)
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| mission_type = [[Communications satellite|Communication]]
| mission_type = [[Communications satellite|Communication]]
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| launch_date = {{start-date|16 February 1999, 01:45:26|timezone=yes}} UTC
| launch_date = {{start-date|16 February 1999, 01:45:26|timezone=yes}} UTC
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| launch_site = [[Cape Canaveral Air Force Station|Cape Canaveral]] [[Spaceport Florida Launch Complex 36|SLC-36A]]
| launch_site = [[Cape Canaveral Air Force Station|Cape Canaveral]] [[Spaceport Florida Launch Complex 36|SLC-36A]]
| launch_contractor = [[International Launch Services|ILS]]
| launch_contractor = [[International Launch Services|ILS]]
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{{DEFAULTSORT:Jcsat-4a}}
{{DEFAULTSORT:Jcsat-4a}}
[[Category:1999 in spaceflight]]
[[Category:Spacecraft launched in 1999]]





Revision as of 13:58, 16 December 2013

Template:No epoch

JCSAT-4A (JCSAT-6)
Mission typeCommunication
OperatorJSAT Corporation
COSPAR ID1999-006A Edit this at Wikidata
SATCAT no.25630Edit this on Wikidata
Mission duration14+12 years (planned)
Spacecraft properties
BusHS-601
ManufacturerHughes
Launch mass2,900 kilograms (6,400 lb)
Start of mission
Launch date16 February 1999, 01:45:26 (1999-02-16UTC01:45:26Z) UTC
RocketAtlas IIAS
Launch siteCape Canaveral SLC-36A
ContractorILS
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Longitude124° East
Perigee altitude35,785 kilometres (22,236 mi)[1]
Apogee altitude35,807 kilometres (22,249 mi)[1]
Inclination0 degrees
Period24 hours
Transponders
Band32 J band
 

JCSAT-4A, previously designated JCSAT-6, is a Japanese geostationary communications satellite which is operated by JSAT Corporation. It is positioned in geostationary orbit at a longitude of 124° East, from where it is used to provide broadcasting and corporate network communications to Japan.[2]

JCSAT-6 was constructed by Hughes, based on the HS-601 satellite bus. It is equipped with 32 J band (IEEE Ku band) transponders, and at launch it had a mass of 2,900 kilograms (6,400 lb), with an expected operational lifespan of fourteen and a half years[3][4]

It was launched atop an Atlas IIAS carrier rocket flying from Space Launch Complex 36A at the Cape Canaveral Air Force Station. The launch occurred at 01:45:26 GMT on 16 February 1999,[5] and successfully placed JCSAT-6 into a geostationary transfer orbit. From this orbit, the satellite raised itself into a geostationary orbit using an R-4D apogee motor.[6] The final burn to complete its insertion into geosynchronous orbit occurred on 1 March 1999.[7]

See also

References

  1. ^ a b McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 2009-08-09.
  2. ^ "JCSAT-4A". Sky Perfect JSAT Corporation. Retrieved 2009-08-08.
  3. ^ "UCS Satellite Database". Union of Concerned Scientists. 2009-07-01. Retrieved 2009-08-08.
  4. ^ Krebs, Gunter. "JCSat 5, 6". Gunter's Space Page. Retrieved 2009-08-08.
  5. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 2009-08-08.
  6. ^ Wade, Mark. "JCSAT". Encyclopedia Astronautica. Retrieved 2009-08-08.
  7. ^ McDowell, Jonathan. "Index". Geostationary Orbit Catalog. Jonathan's Space Page. Retrieved 2009-08-08.