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Astra 1G
Mission type Communications
Operator Société Européenne des Satellites / SES S.A.
COSPAR ID 1997-076A Edit this at Wikidata
SATCAT no.25071
Website https://www.ses.com/
Mission durationPlanned: 15 years
Final: 25 years and 6 months
Spacecraft properties
Spacecraft type Boeing 601HP
Bus HS-601HP
Manufacturer Hughes Space and Communications
Launch mass3,379 kg (7,449 lb)
Power6 kW
Start of mission
Launch date2 December 1997, 23:10:37 UTC
Rocket Proton-K / DM-2M
Launch site Baikonur, Site 81/23
Contractor Khrunichev State Research and Production Space Center
Entered serviceFebruary 1998
End of mission
Disposal Graveyard orbit
DeactivatedJune 2023
Orbital parameters
Reference system Geocentric orbit [1]
Regime Geostationary orbit
Longitude Astra 19.2° East (1997-2009)
Astra 23.5° East (2009-2010)
Astra 31.5° East (2010-2014)
60° East (2014-2016)
63° East (2016-2017)
51° East (2017-2018)
57° East (2018-2019)
63° East (2019-2021)
Astra 19.2° East (2021-2023)
Transponders
Band32 Ku-band
Coverage areaEurope
←  Astra 1F
Astra 2A →
 

Astra 1G was one of the Astra communications satellites owned and operated by SES.

History

SES ordered its Hughes 601HP satellite, in 1994 for Astra 1G. [2]

Astra 1G was retired to a graveyard orbit in 2023. [3]

Launch

Astra-1G was launched on 2 December 1997 at 23:10:37 UTC, by a Proton-K / DM-2M launch vehicle, from Site 81/23 at the Baikonur Cosmodrome in Kazakhstan. It was maneuvered into a geostationary orbit and at 19.2° East of longitude. [4]

See also

  • SES (satellite operator)
  • Astra (satellite family)

References

  1. ^ "ASTRA 1G". N2YO.com. Retrieved 7 April 2021.
  2. ^ "Astra 1G, 1H, 2A, 2C". Gunter's Space Page. 11 December 2017. Retrieved 7 April 2021.
  3. ^ Real Time Satellite Tracking And Predictions Accessed 29 June 26 2023
  4. ^ "Satellites". Heavens Above. 7 April 2021. Retrieved 7 April 2021.

External links