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| dbo:abstract
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- INSAT-4B was an Indian communications satellite which forms part of the Indian National Satellite System. Launched in 2007, it was placed in geostationary orbit at a longitude of 93.48° East. Built by the Indian Space Research Organisation, INSAT-4B is based upon the I-3K satellite bus. It had a mass at launch of 3,028 kilograms (6,676 lb), with a dry mass of 1,335 kilograms (2,943 lb) and was expected to operate for twelve years. Two solar arrays power the satellite, while its communications payload consists of twelve C and twelve Ku band transponders. Arianespace was contracted to launch INSAT-4B using an Ariane 5 ECA carrier rocket. The launch occurred on 11 March 2007 at 22:03 UTC, from ELA-3 at Kourou. The Skynet 5A military communications satellite for the British Ministry of Defence was launched aboard the same rocket. INSAT-4B was successfully inserted into geosynchronous transfer orbit, from which it raised itself into geostationary orbit using a liquid-fuelled apogee motor. It received the International Designator 2007-007A and Satellite Catalog Number 30793. As of 11 November 2013, it is in an orbit with a perigee of 35,776 kilometres (22,230 mi), an apogee of 35,809 kilometres (22,251 mi), inclination of 0.07 degrees and an orbital period of 23.93 hours. (en)
- O INSAT-4B é um satélite de comunicação geoestacionário indiano da série INSAT que está localizado na posição orbital de 93,5 graus de longitude leste, ele foi construído e também é operado pela Organização Indiana de Pesquisa Espacial (ISRO). O INSAT-4B é idêntico ao INSAT-4A. O satélite foi baseado na plataforma e sua expectativa de vida útil é de 12 anos. (pt)
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| dbo:launchDate
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| dbo:missionDuration
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- 378691200.000000 (xsd:double)
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| dbo:operator
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| dbo:satcat
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| dbo:type
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| dbo:wikiPageID
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- 8031 (xsd:nonNegativeInteger)
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| dbo:wikiPageRevisionID
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| dbo:wikiPageWikiLink
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| dbp:apsis
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| dbp:cosparId
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| dbp:deactivated
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| dbp:disposalType
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| dbp:launchContractor
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| dbp:launchDate
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- 0001-03-11 (xsd:gMonthDay)
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| dbp:launchRocket
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| dbp:launchSite
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| dbp:manufacturer
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| dbp:missionDuration
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- 0001-03-11 (xsd:gMonthDay)
- 3.786912E8 (dbd:second)
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| dbp:missionType
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| dbp:name
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| dbp:operator
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| dbp:orbitEccentricity
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| dbp:orbitEpoch
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- 0001-11-11 (xsd:gMonthDay)
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| dbp:orbitInclination
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| dbp:orbitLongitude
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- 83 (xsd:integer)
- 85.500000 (xsd:double)
- 93.480000 (xsd:double)
- 111.200000 (xsd:double)
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| dbp:orbitPeriod
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| dbp:orbitReference
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| dbp:orbitRegime
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| dbp:power
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| dbp:satcat
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| dbp:spacecraftBus
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| dbp:wikiPageUsesTemplate
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| rdfs:comment
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- O INSAT-4B é um satélite de comunicação geoestacionário indiano da série INSAT que está localizado na posição orbital de 93,5 graus de longitude leste, ele foi construído e também é operado pela Organização Indiana de Pesquisa Espacial (ISRO). O INSAT-4B é idêntico ao INSAT-4A. O satélite foi baseado na plataforma e sua expectativa de vida útil é de 12 anos. (pt)
- INSAT-4B was an Indian communications satellite which forms part of the Indian National Satellite System. Launched in 2007, it was placed in geostationary orbit at a longitude of 93.48° East. Built by the Indian Space Research Organisation, INSAT-4B is based upon the I-3K satellite bus. It had a mass at launch of 3,028 kilograms (6,676 lb), with a dry mass of 1,335 kilograms (2,943 lb) and was expected to operate for twelve years. Two solar arrays power the satellite, while its communications payload consists of twelve C and twelve Ku band transponders. (en)
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| rdfs:label
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- INSAT-4B (en)
- INSAT-4B (pt)
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