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Astra 1F
Mission type Communications
Operator SES
COSPAR ID 1996-021A Edit this at Wikidata
SATCAT no.23842
Website https://www.ses.com/
Mission duration15 years (planned)
24 years, 7 months (achieved)
Spacecraft properties
Spacecraft type Boeing 601
Bus HS-601
Manufacturer Hughes Space and Communications
Launch mass3,010 kg (6,640 lb)
Power4.7 kW
Start of mission
Launch date8 April 1996, 23:09:01 UTC
Rocket Proton-K / DM-2M
Launch site Baikonur, Site 81/23
Contractor Khrunichev State Research and Production Space Center
Entered serviceJune 1996
End of mission
Disposal Graveyard orbit
DeactivatedNovember 2020
Orbital parameters
Reference system Geocentric orbit [1]
Regime Geostationary orbit
Longitude19.2° East
Transponders
Band16 Ku-band
BandwidthFSS: 26 Mhz
BSS: 33 MHz
Coverage areaEurope
←  Astra 1E
Astra 1G →
 

Astra 1F is one of the Astra communications satellites in geostationary orbit owned and operated by SES. It was launched in April 1996 to the Astra 19.2°E orbital slot initially to provide digital television and radio for direct-to-home (DTH) across Europe.

The satellite originally provided two broadcast beams, of horizontal and vertical polarisation, for Fixed Service Satellite (FSS) (10.70-10.95 GHz) and for Broadcast Satellite Service (BSS) (11.70-12.10 GHz) frequency bands. The FSS beams provide footprints that 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

References

  1. ^ "ASTRA 1F". www.n2yo.com. Retrieved 7 April 2021.
  2. ^ "Astra 1E, 1F". space.skyrocket.de. Gunter's Space Page. 11 December 2017. Retrieved 7 April 2021.

External links