About: INSAT-1B

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INSAT-1B was an Indian communications satellite which formed part of the Indian National Satellite System. Launched in 1983, it was operated in geostationary orbit at a longitude of 74 degrees east. At the end of its seven-year design life it was replaced by the newly launched INSAT-1D, dropping to backup status. In 1992, it was relocated to 93° east, before being decommissioned in August 1993.

Attributes	Values
rdf:type	Thing schema:Event dul:Event societal event wikidata:Q1656682 wikidata:Q2133344 yago:Abstraction100002137 yago:Act100030358 yago:Action100037396 yago:Change100191142 yago:Event100029378 yago:Journey100306426 yago:Motion100279835 yago:PsychologicalFeature100023100 yago:YagoPermanentlyLocatedEntity event space mission yago:Spaceflight100313502 yago:Travel100295701 yago:Voyage100312553 ArtificialSatellite
rdfs:label	INSAT-1B (en) INSAT-1B (pt)
rdfs:comment	O INSAT-1B foi um satélite de comunicação e meteorológico geoestacionário indiano da série INSAT que foi construído pela Ford Aerospace. Ele esteve localizado na posição orbital de 74 graus de longitude leste e era operado pela Organização Indiana de Pesquisa Espacial (ISRO). O satélite foi baseado na plataforma e sua vida útil estimada é de 7 anos. O mesmo saiu de serviço em agosto de 1993. (pt) INSAT-1B was an Indian communications satellite which formed part of the Indian National Satellite System. Launched in 1983, it was operated in geostationary orbit at a longitude of 74 degrees east. At the end of its seven-year design life it was replaced by the newly launched INSAT-1D, dropping to backup status. In 1992, it was relocated to 93° east, before being decommissioned in August 1993. (en)
foaf:name	INSAT-1B (en)
name	INSAT-1B (en)
foaf:depiction
dct:subject	1983 in India 1983 in spaceflight Spacecraft launched in 1983 INSAT satellites
Wikipage page ID	23733824 (xsd:integer)
Wikipage revision ID	1063687881 (xsd:integer)
Link from a Wikipage to another Wikipage	Apsis Indian National Satellite System International Designator STS-8 S band Geocentric orbit Geostationary orbit NASA 1983 in India 1983 in spaceflight Communications satellite Orbital period Payload Assist Module C band (IEEE) Spacecraft launched in 1983 Ford Aerospace Graveyard orbit Kennedy Space Center Kennedy Space Center Launch Complex 39 Apogee motor R-4D Satellite bus Orbital inclination Satellite Catalog Number INSAT satellites Geosynchronous transfer orbit INSAT Solar array
sameAs	INSAT-1B INSAT-1B INSAT-1B INSAT-1B INSAT-1B INSAT-1B INSAT-1B
dbp:wikiPageUsesTemplate	dbt:INSAT_Satellites dbt:Convert dbt:Infobox_spaceflight dbt:Portal dbt:Reflist dbt:End-date dbt:Start-date dbt:OV dbt:Orbital_launches_in_1983 dbt:Indian_spacecraft
thumbnail	wiki-commons:Special:FilePath/Insat-1B.jpg?width=300
apsis	gee (en)
COSPAR ID	1983 (xsd:integer)
image caption	INSAT-1B before launch (en)
launch contractor	NASA
launch date	0001-08-30 (xsd:gMonthDay)
launch rocket	STS-8 Payload Assist Module
launch site	Kennedy Space Center Kennedy Space Center Launch Complex 39
manufacturer	Ford Aerospace
mission duration	2.209032E8 (second)
mission type	Communications satellite
operator	INSAT
orbit inclination	14.690000 (xsd:double)
orbit period	86148.0 (second)
orbit reference	Geocentric orbit
orbit regime	Geostationary orbit
SATCAT	14318 (xsd:integer)
spacecraft type	INSAT-1 (en)
has abstract	INSAT-1B was an Indian communications satellite which formed part of the Indian National Satellite System. Launched in 1983, it was operated in geostationary orbit at a longitude of 74 degrees east. At the end of its seven-year design life it was replaced by the newly launched INSAT-1D, dropping to backup status. In 1992, it was relocated to 93° east, before being decommissioned in August 1993. Built by Ford Aerospace and operated by the Indian National Satellite System, INSAT-1B was based upon a custom satellite bus developed for the INSAT-1 series of satellites. It had a mass at launch of 1,152 kilograms (2,540 lb), and was expected to operate for seven years. The spacecraft carried twelve C and three S band transponders, powered by a single solar array. A stabilisation boom was used to counterbalance radiation torques from the satellite's asymmetrical design. The spacecraft was propelled by an R-4D-11 apogee motor. INSAT-1B was deployed by Space Shuttle Challenger during the STS-8 mission. Challenger lifted off from Launch Complex 39A at the Kennedy Space Center at 06:32:00 UTC on 30 August 1983. INSAT-1B was deployed from the orbiter's payload bay at 07:48 UTC on 31 August, with a PAM-D upper stage firing shortly afterwards to place it into geosynchronous transfer orbit. The spacecraft used its own propulsion system to raise itself into geostationary orbit. It received the International Designator 1983-089B and Satellite Catalog Number 14318. After some initial problems deploying its solar array, INSAT-1B became operational in October 1983. It was located at 74° east for most of its operational life, before being moved to 93° east in 1992. In August 1993 it was decommissioned and raised to a graveyard orbit slightly above geosynchronous altitude. As of 14 November 2013, it is in an orbit with a perigee of 35,741 kilometres (22,208 mi), an apogee of 35,846 kilometres (22,274 mi), inclination of 14.69 degrees and an orbital period of 23.93 hours. (en)

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