Eurasiasat 1 (Türksat 2A) [Thales Alenia Space]
The satellite Eurasiasat 1 (also known as Türksat 2A) is positioned at 42°E, where it is co-located with Türksat 1C. The satellite is operated by Eurasiasat SAM, Monaco.
The 3535 kg spacecraft was built by Alcatel Space Industries using a Spacebus-3000B3 satellite bus. The satellite is equipped with 32 Ku-band transponders, and has an expected design life of 12 years.
The satellite was retired in 2016 and was moved into a graveyard orbit above the geostationary belt.
Nation: | Türkiye (Turkey) |
---|---|
Type / Application: | Communication |
Operator: | Eurasiasat SAM / Türksat AS |
Contractors: | Aerospatiale |
Equipment: | 32 Ku-band transponders |
Configuration: | Spacebus-3000B3 |
Propulsion: | S400 |
Power: | 2 deployable solar arrays, batteries |
Lifetime: | 12 years |
Mass: | 3535 kg |
Orbit: | GEO |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
---|---|---|---|---|---|---|
Eurasiasat 1 (Türksat 2A) | 2001-002A | 10.01.2001 | Ko ELA-2 | Ariane-44P H10-3 |