AsiaSat 3S

AsiaSat 3S
Mission typeCommunications
OperatorAsiaSat
COSPAR ID1999-013A Edit this at Wikidata
SATCAT no.25657
Mission duration15 years (planned)
25 years, 7 months and 23 days (in progress)
Spacecraft properties
SpacecraftAsiaSat 3S
Spacecraft typeBoeing 601
BusHS-601HP
ManufacturerHughes Space and Communications
Launch mass3,480 kg (7,670 lb)
Dry mass2,500 kg (5,500 lb)
Dimensions3.4 m x 3.5 m x 5.8 m
Span: 26.2 m on orbit
Power9.9 kW
Start of mission
Launch date21 March 1999, 00:09:30 UTC
RocketProton-K / DM-2M
Launch siteBaikonur, Site 81/23
ContractorKhrunichev State Research and Production Space Center
Entered service8 May 1999
Orbital parameters
Reference systemGeocentric orbit
RegimeGeostationary orbit
Longitude105.5° East (1999–2014)
120° East (2014–2015)
150.5° East (2015–2016)
146° East (2016–2019) [1]
Transponders
Band44 transponders:
28 C-band
16 Ku-band
Coverage areaAsia, the Middle East and Oceania

AsiaSat 3S, was a geosynchronous communications satellite for AsiaSat of Hong Kong to provide communications and television services all across Asia, the Middle East and Oceania.

  1. ^ Cite error: The named reference TSE was invoked but never defined (see the help page).