AsiaSat 5
| Mission type | Communications |
|---|---|
| Operator | AsiaSat |
| COSPAR ID | 2009-042A |
| SATCAT no. | 35696 |
| Website | https://www.asiasat.com |
| Mission duration | 15 years (planned) 15 years, 2 months and 16 days (in progress) |
| Spacecraft properties | |
| Spacecraft | AsiaSat 5 |
| Spacecraft type | SSL 1300 |
| Bus | LS-1300SX |
| Manufacturer | Space Systems/Loral |
| Launch mass | 3,760 kg (8,290 lb) |
| Start of mission | |
| Launch date | 11 August 2009, 19:47:33 UTC |
| Rocket | Proton-M / Briz-M |
| Launch site | Baikonur, Site 200/39 |
| Contractor | Khrunichev State Research and Production Space Center |
| Entered service | October 2009 |
| Orbital parameters | |
| Reference system | Geocentric orbit[1] |
| Regime | Geostationary orbit |
| Longitude | 100.5° East |
| Transponders | |
| Band | 40 transponders: 26 C-band 14 Ku-band |
| Coverage area | Asia, Pacific Ocean region |
AsiaSat 5 is a Hong Kong communications satellite, which is operated by the Hong Kong–based Asia Satellite Telecommunications Company (AsiaSat). It is positioned in geostationary orbit at a longitude of 100.5° East of the Greenwich Meridian, where it replaced the AsiaSat 2 satellite.[2] It is used to provide fixed satellite services, including broadcasting, telephone and broadband very small aperture terminal (VSAT) communications, to Asia and the Pacific Ocean region.[3]
Background
[edit]The launch was originally scheduled to be conducted by Land Launch (SSL-1300LL satellite bus), using a Zenit-3SLB launch vehicle. The satellite was subsequently re-awarded to ILS after Land Launch were unable to guarantee that the satellite could be launched by August 2009, in order to be in orbit before AsiaSat 2 ceased operations.[4][5]
Satellite description
[edit]Space Systems/Loral (SS/L), announced in May 2005 that it has been chosen by AsiaSat. At launch, AsiaSat 5 had a mass of 3,760 kg (8,290 lb),[6] and was expected to operate for fifteen years. It carries 26 C-band and 14 Ku-band transponders.[2]
Launch
[edit]AsiaSat 5 was built by Space Systems/Loral, and is based on the LS-1300XS satellite bus.[3] It is being launched by International Launch Services (ILS), using a Proton-M launch vehicle with a Briz-M upper stage. The launch was conducted from Site 200/39 at the Baikonur Cosmodrome in Kazakhstan, at 19:47:33 UTC on 11 August 2009. The Briz-M separated from the Proton-M nine minutes and forty one seconds into the flight, and AsiaSat 5 will separate from the Briz-M into a geosynchronous transfer orbit (GTO) nine hours and fifteen minutes after liftoff.[6] It will then raise itself into its final geostationary orbit.
See also
[edit]
References
[edit]- ^ "ASIASAT 5". N2YO.com. Retrieved 5 May 2021.
- ^ a b "Satellite Fleet - AsiaSat 5". AsiaSat. Retrieved 5 May 2021.
- ^ a b Krebs, Gunter (11 December 2017). "AsiaSat 5, 7 / Thaicom 6A". Gunter's Space Page. Retrieved 5 May 2021.
- ^ "ILS Announces 9 New Proton Missions in First Half of 2009". Reuters. 15 June 2009. Archived from the original on 5 March 2016. Retrieved 5 May 2021.
- ^ Clark, Stephen (3 April 2009). "Multi-tasking satellite deployed by 50th ILS Proton". Spaceflight Now. Retrieved 11 August 2009.
- ^ a b "Mission Overview - AsiaSat 5" (PDF). International Launch Services. Retrieved 2 August 2009.