Names | AsiaSat 3 HGS-1 PAS-22 |
---|---|
Mission type | Communications |
Operator | AsiaSat (1997–1998) Hughes (1998–1999) PanAmSat (1999–2002) |
COSPAR ID | 1997-086A |
SATCAT no. | 25126 |
Mission duration | 15 years (planned) [1]
4 years (achieved) |
Spacecraft properties | |
Spacecraft | AsiaSat 3 |
Spacecraft type | Boeing 601 |
Bus | HS-601HP |
Manufacturer | Hughes Space and Communications |
Launch mass | 3,465 kg[2] |
Dry mass | 2,500 kg (5,500 lb) |
Dimensions | 3.4 m x 3.5 m x 5.8 m Span: 26.2 m on orbit |
Power | 9.9 kW |
Start of mission | |
Launch date | 24 December 1997, 23:19:00 UTC[3] |
Rocket | Proton-K / DM-2M |
Launch site | Baikonur, Site 81/23 |
Contractor | Khrunichev State Research and Production Space Center |
Entered service | July 1998 |
End of mission | |
Disposal | Graveyard orbit |
Deactivated | July 2002 |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Longitude | 105.5° East (intended) 158° West (1998-1999) 62° West (1999–2002) [4] |
Flyby of Moon | |
Closest approach | 13 May 1998, 19:00 UTC [5] |
Distance | 6,200 km (3,900 mi) |
Flyby of Moon | |
Closest approach | 6 June 1998, 16:30 UTC |
Distance | 34,300 km (21,300 mi) |
Transponders | |
Band | 44 transponders: 28 C-band 16 Ku-band |
Coverage area | Asia |
AsiaSat 3, previously known as HGS-1 and then PAS-22, was a geosynchronous communications satellite, which was salvaged from an unusable geosynchronous transfer orbit (GTO) by means of the Moon's gravity.
TSE
was invoked but never defined (see the help page).