Palapa-C2

Palapa-C2
Mission typeCommunications
OperatorPT Satelit Palapa Indonesia (SATELINDO)
COSPAR ID1996-030A Edit this at Wikidata
SATCAT no.23864
Websitehttps://indosatooredoo.com/
Mission duration15 years (planned)
20 years (achieved)
Spacecraft properties
SpacecraftPalapa-C2
Spacecraft typeBoeing 601
BusHS-601
ManufacturerHughes Space and Communications Company
Launch mass3,014 kg (6,645 lb)
Dry mass1,740 kg (3,840 lb)
DimensionsSpan: 21 m (69 ft)
Power3730 watts
Start of mission
Launch date16 May 1996, 01:56:29 UTC
RocketAriane 44L H10-3 (V86)
Launch siteCentre Spatial Guyanais, Kourou, ELA-2
ContractorArianespace
Entered serviceJuly 1996
End of mission
DisposalGraveyard orbit
DeactivatedNovember 2016
Orbital parameters
Reference systemGeocentric orbit
RegimeGeostationary orbit
Longitude113° East (1996-2009)
150.5° East (2009-2014)
146° East (2014-2016)
Transponders
Band34 transponders:
30 C-band
4 Ku-band
Coverage areaIndonesia, Southeast Asia, parts of China, India, Japan, Australia

Palapa-C2 was an Indonesian communications satellite which reached its target orbit on 16 May 1996. It was built by Hughes Space and Communications Company (now Boeing Satellite Development Center) for Indonesian telecommunications provider PT Satelit Palapa Indonesia (SATELINDO). It was based on the HS-601 satellite bus and had 30 C-band transponders and 4 Ku-band transponders. It was due to be located in geosynchronous orbit at 113° East above the equator. It operated for more than 20 years, more than five years past the designed life time of 15 years, making it the longest operation among the Indonesian fleet of communications satellites.