Astra 1F
Mission type | Communications |
---|---|
Operator | SES |
COSPAR ID | 1996-021A |
SATCATno. | 23842 |
Website | https://www.ses.com/ |
Mission duration | 15 years (planned) 24 years, 7 months (achieved) |
Spacecraft properties | |
Spacecraft type | Boeing 601 |
Bus | HS-601 |
Manufacturer | Hughes Space and Communications |
Launch mass | 3,010 kg (6,640 lb) |
Power | 4.7kW |
Start of mission | |
Launch date | 8 April 1996, 23:09:01UTC |
Rocket | Proton-K/DM-2M |
Launch site | Baikonur,Site 81/23 |
Contractor | Khrunichev State Research and Production Space Center |
Entered service | June 1996 |
End of mission | |
Disposal | Graveyard orbit |
Deactivated | November 2020 |
Orbital parameters | |
Reference system | Geocentric orbit[1] |
Regime | Geostationary orbit |
Longitude | 19.2° East |
Transponders | |
Band | 16Ku-band |
Bandwidth | FSS: 26Mhz BSS: 33 MHz |
Coverage area | Europe |
Astra 1Fis one of theAstracommunications satellitesingeostationary orbitowned and operated bySES.It was launched in April 1996 to theAstra 19.2°Eorbital slot initially to provide digital television and radio fordirect-to-home(DTH) across Europe.
The satellite originally provided two broadcast beams, of horizontal and verticalpolarisation,forFixed Service Satellite(FSS) (10.70-10.95GHz) and forBroadcast Satellite Service(BSS) (11.70-12.10 GHz) frequency bands. The FSS beams providefootprintsthat cover essentially the same area of Europe – northern, central and eastern Europe, including Spain and northern Italy – while the BSS horizontal beam excludes Spain and extends further east, and the BSS vertical beam includes Spain and more of southern Italy but does not extend so far east. Within the footprints, television signals are usually received with a 60–80 cm dish.[2]
See also
[edit]- Astrasatellite family
- SES(operator)
- SES BroadbandInternet service
References
[edit]- ^"ASTRA 1F".www.n2yo.com.Retrieved7 April2021.
- ^"Astra 1E, 1F".space.skyrocket.de.Gunter's Space Page. 11 December 2017.Retrieved7 April2021.