Mission type | Communications |
---|---|
Operator | PT Telkom |
COSPAR ID | 2005-046A |
SATCAT no. | 28902 |
Website | https://www.telkom.co.id/sites |
Mission duration | 15 years (planned) 15 years, 6 months and 19 days (final) |
Spacecraft properties | |
Spacecraft | Telkom-2[1] |
Spacecraft type | Star-2 |
Bus | GEOStar-2 |
Manufacturer | Orbital Sciences Corporation |
Launch mass | 1,975 kg (4,354 lb) |
Dry mass | 899 kg (1,982 lb) |
Dimensions | 2.4 m x 3.3 m x 1.9 m Span on orbit: 12.6 m |
Power | 2.918 kW |
Start of mission | |
Launch date | 16 November 2005, 23:46:00 UTC[2] |
Rocket | Ariane 5ECA (V167) |
Launch site | Centre Spatial Guyanais, Kourou, ELA-3 |
Contractor | Arianespace |
Entered service | January 2006 |
End of mission | |
Disposal | Graveyard orbit |
Deactivated | 4 June 2021 |
Orbital parameters | |
Reference system | Geocentric orbit[3] |
Regime | Geostationary orbit |
Longitude | 118° East 157° East |
Transponders | |
Band | 24 C-band |
Coverage area | Indonesia, Southeast Asia, Indian subcontinent |
Telkom-2 was a geosynchronous communications satellite built by Orbital Sciences Corporation (OSC) for Indonesia's state-owned telecommunications company, PT Telekomunikasi Indonesia Tbk (PT Telkom). Telkom-2 was successfully launched on 16 November 2005, at 23:46:00 UTC and positioned in geostationary orbit, at 118° East for replaced Palapa-B4.