Turksat 1B was a Turkish communications satellite as part of a project to form an instant network with two geosynchronous satellites that is supervised by the companies Türksat A.Ş. in Turkey and Aérospatiale of France.
Mission type | Communication |
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Operator | Türksat |
COSPAR ID | 1994-049B[1] |
SATCAT no. | 23200[1] |
Spacecraft properties | |
Bus | Spacebus 2000 |
Manufacturer | Aérospatiale |
Start of mission | |
Launch date | August 10, 1994, 23:05 (1994-08-10UTC23:05Z) UTC |
Rocket | Ariane 44LP H10+ |
Launch site | Kourou ELA-2 |
End of mission | |
Deactivated | October 17, 2006 (2006-10-18) |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 42°E |
Transponders | |
Band | 16 Ku band |
Türksat program |
Türksat 1B was launched by Arianespace atop an Ariane-44LP H10+ launch vehicle, along with Brazilian satellite Brasilsat B1, in a dual-payload launch on August 10, 1994, at 23:05 UTC from ELA-2 at the Guiana Space Centre in Kourou, French Guiana. The satellite was successfully placed into geostationary transfer orbit and positioned at 42°E.[1][2][3][4]
It is based on the Aerospatiale Spacebus 2000 series having an on-orbit mass of about one ton. The communications payload consists of 16 Ku band transponders with six wideband channels of 72 MHz and ten narrowband of 36 MHz.[2]
In addition to Turkey, the satellite covered a geographical range from Europe to Central Asia before completing its mission in 2006.[4]
← 1993 · Orbital launches in 1994 · 1995 → | |
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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Cubesats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses). |
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