Astra 1G

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Astra 1G
Mission type Communications
Operator SES
COSPAR ID 1997-076A OOjs UI icon edit-ltr-progressive.svg
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.

Contents

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

Related Research Articles

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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.