GSAT-8
GSAT-8
GSAT-8 |
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Mission type |
Communication |
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Operator |
ISRO |
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COSPAR ID |
2011-022A |
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Mission duration |
12 Years |
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Spacecraft properties |
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Bus |
I-3K |
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Manufacturer |
ISRO |
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Launch mass |
3,093 kilograms (6,819 lb) |
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Dry mass |
1,426 kilograms (3,144 lb) |
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Power |
6,242 watts |
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Start of mission |
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Launch date |
20 May 2011, 20:38 (2011-05-20UTC20:38Z) UTC |
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Rocket |
Ariane 5ECA VA202 |
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Launch site |
Kourou ELA-3 |
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Contractor |
Arianespace |
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Orbital parameters |
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Reference system |
Geocentric |
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Regime |
Geostationary |
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Longitude |
55° East |
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Transponders |
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Band |
24 Ku band |
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GSAT-8 is communication satellite. It was constructed by the Indian Space Research Organisation, as part of INSAT system. GSAT-8 was launched on May 21, 2011 from Kourou, French Guiana. The rocket, an Ariane 5 was the carrier, marketed by the European Arianespace.
Launch
Prior to launch, the spacecraft was transported from India to Cayenne – Rochambeau Airport in French Guiana by an Antonov An-124 cargo aircraft. The success of the launch is said to have made up for the previous loss of two satellites on the indigenous GSLV rocket.[1][2]
References
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| Past | |
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| Current | |
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| Future | |
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| Signs † indicate launch failures. |
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| INSAT-1 Series | |
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| INSAT-2 Series | |
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| INSAT-3 Series | |
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| INSAT-4 Series | |
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| | | Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets). |
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