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	<title>INSAT-1B - Revision history</title>
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	<updated>2026-07-30T12:13:02Z</updated>
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		<id>https://indianpedia.org/index.php?title=INSAT-1B&amp;diff=424654&amp;oldid=prev</id>
		<title>Ajay Kumar at 07:50, 2 September 2023</title>
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		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;{{Infobox spaceflight&lt;br /&gt;
| name                  = INSAT-1B&lt;br /&gt;
| image                 = Insat-1B.jpg&lt;br /&gt;
| image_caption         = INSAT-1B before launch&lt;br /&gt;
&lt;br /&gt;
| mission_type          = [[Communications satellite|Communications]]&lt;br /&gt;
| operator              = [[INSAT]]&lt;br /&gt;
| COSPAR_ID             = 1983-089B&lt;br /&gt;
| SATCAT                = 14318&lt;br /&gt;
| mission_duration      = 7&amp;amp;nbsp;years&lt;br /&gt;
&lt;br /&gt;
| spacecraft_type       = [[INSAT]]-1&lt;br /&gt;
| manufacturer          = [[Ford Aerospace]]&lt;br /&gt;
| launch_mass           = {{convert|1152|kg|lb}}&lt;br /&gt;
| dry_mass              = &lt;br /&gt;
| power                 =&lt;br /&gt;
&lt;br /&gt;
| launch_date           = 30 August 1983, 06:32:00&amp;amp;nbsp;UTC&amp;lt;ref name=&amp;quot;launchlog&amp;quot;&amp;gt;{{cite web|url=http://planet4589.org/space/log/launchlog.txt|title=Launch Log|first=Jonathan|last=McDowell|work=Jonathan&amp;#039;s Space Page|access-date=16 November 2013}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
| launch_rocket         = {{OV|099}}&amp;lt;br/&amp;gt;[[STS-8]] / [[Payload Assist Module|PAM-D]]&lt;br /&gt;
| launch_site           = [[Kennedy Space Center|Kennedy]] [[Kennedy Space Center Launch Complex 39|LC-39A]]&lt;br /&gt;
| launch_contractor     = [[NASA]]&lt;br /&gt;
| deployment_date       = {{start-date|31 August 1983, 07:48|timezone=yes}}&amp;amp;nbsp;UTC&lt;br /&gt;
| entered_service       =&lt;br /&gt;
&lt;br /&gt;
| disposal_type         = Decommissioned&lt;br /&gt;
| deactivated           = {{end-date|August 1993}}&lt;br /&gt;
&lt;br /&gt;
| orbit_epoch           = 14 November 2013, 15:52:38&amp;amp;nbsp;UTC&amp;lt;ref name=&amp;quot;n2yo&amp;quot;&amp;gt;{{cite web|url=http://www.n2yo.com/satellite/?s=14318|title=INSAT 1B Satellite details 1983-089B NORAD 14318|work=N2YO|date=14 November 2013|access-date=16 November 2013}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
| orbit_reference       = [[Geocentric orbit|Geocentric]]&lt;br /&gt;
| orbit_regime          = [[Geostationary orbit|Geostationary]]&lt;br /&gt;
| orbit_periapsis       = {{convert|35741|km|mi}}&lt;br /&gt;
| orbit_apoapsis        = {{convert|35846|km|mi}}&lt;br /&gt;
| orbit_inclination     = 14.69&amp;amp;nbsp;degrees&lt;br /&gt;
| orbit_semimajor       = {{convert|42164.88|km|mi}}&lt;br /&gt;
| orbit_eccentricity    = 0.0012393&lt;br /&gt;
| orbit_period          = 23.93&amp;amp;nbsp;hours&lt;br /&gt;
| orbit_longitude       = 74°&amp;amp;nbsp;east (1983-92)&amp;lt;br/&amp;gt;93°&amp;amp;nbsp;east (1992-93)&lt;br /&gt;
| apsis                 = gee&lt;br /&gt;
}}&lt;br /&gt;
&amp;#039;&amp;#039;&amp;#039;INSAT-1B&amp;#039;&amp;#039;&amp;#039; 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.&amp;lt;ref name=&amp;quot;GSP&amp;quot;/&amp;gt; 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.&amp;lt;ref name=&amp;quot;GSP&amp;quot;&amp;gt;{{cite web|url=http://space.skyrocket.de/doc_sdat/insat-1a.htm|title=Insat 1A, 1B, 1C, 1D|first=Gunter|last=Krebs|work=Gunter&amp;#039;s Space Page|access-date=16 November 2013}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Built by [[Ford Aerospace]] and operated by the [[Indian National Satellite System]],&amp;lt;ref name=&amp;quot;GSP&amp;quot; /&amp;gt; INSAT-1B was based upon a custom [[satellite bus]] developed for the [[INSAT]]-1 series of satellites. It had a mass at launch of {{convert|1152|kg}}, and was expected to operate for seven years. The spacecraft carried twelve [[C band (IEEE)|C]] and three [[S band]] transponders, powered by a single [[solar array]].&amp;lt;ref name=&amp;quot;GSP&amp;quot;/&amp;gt; A stabilisation boom was used to counterbalance radiation torques from the satellite&amp;#039;s asymmetrical design.&amp;lt;ref name=&amp;quot;SSF302&amp;quot;&amp;gt;{{cite book|last=Harland|first=David M|author2=Lorenz, Ralph D.|title=Space Systems Failures|publisher=Springer-Praxis|location=Chichester|year=2005|edition=2006|isbn=0-387-21519-0|pages=302–3}}&amp;lt;/ref&amp;gt; The spacecraft was propelled by an [[R-4D|R-4D-11]] [[apogee motor]].&lt;br /&gt;
&lt;br /&gt;
INSAT-1B was deployed by {{OV|099}} during the [[STS-8]] mission. &amp;#039;&amp;#039;Challenger&amp;#039;&amp;#039; lifted off from [[Kennedy Space Center Launch Complex 39|Launch Complex 39A]] at the [[Kennedy Space Center]] at 06:32:00 UTC on 30 August 1983.&amp;lt;ref name=&amp;quot;launchlog&amp;quot;/&amp;gt; INSAT-1B was deployed from the orbiter&amp;#039;s payload bay at 07:48 UTC on 31 August, with a [[Payload Assist Module|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.&amp;lt;ref name=&amp;quot;satcat&amp;quot;&amp;gt;{{cite web|url=http://planet4589.org/space/log/satcat.txt|title=Satellite Catalog|first=Jonathan|last=McDowell|work=Jonathan&amp;#039;s Space Page|access-date=16 November 2013}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
After some initial problems deploying its solar array,&amp;lt;ref name=&amp;quot;SSF234&amp;quot;&amp;gt;{{cite book|last=Harland|first=David M|author2=Lorenz, Ralph D.|title=Space Systems Failures|publisher=Springer-Praxis|location=Chichester|year=2005|edition=2006|isbn=0-387-21519-0|page=234}}&amp;lt;/ref&amp;gt; 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.&amp;lt;ref name=&amp;quot;GSP&amp;quot;/&amp;gt; As of 14 November 2013, it is in an orbit with a [[apsis|perigee]] of {{convert|35741|km|mi}}, an [[apsis|apogee]] of {{convert|35846|km|mi}}, [[orbital inclination|inclination]] of 14.69&amp;amp;nbsp;degrees and an [[orbital period]] of 23.93&amp;amp;nbsp;hours.&amp;lt;ref name=&amp;quot;n2yo&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==References==&lt;br /&gt;
{{Portal|Spaceflight}}&lt;br /&gt;
{{reflist}}&lt;br /&gt;
&lt;br /&gt;
{{INSAT Satellites}}&lt;br /&gt;
{{Indian spacecraft}}&lt;br /&gt;
{{Orbital launches in 1983}}&lt;br /&gt;
&lt;br /&gt;
[[Category:INSAT satellites]]&lt;br /&gt;
[[Category:1983 in India]]&lt;br /&gt;
[[Category:1983 in spaceflight]]&lt;br /&gt;
[[Category:Spacecraft launched in 1983]]&lt;/div&gt;</summary>
		<author><name>Ajay Kumar</name></author>
	</entry>
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