From Wikipedia, the free encyclopedia

Astra 1L
Mission type Communications
Operator SES
COSPAR ID 2007-016A Edit this at Wikidata
SATCAT no.31306
Website https://www.ses.com/
Mission duration15 years (planned)
16 years, 11 months, 23 days (elapsed)
Spacecraft properties
Spacecraft type Lockheed Martin A2100 [1]
Bus A2100AXS
Manufacturer Lockheed Martin
Launch mass4,497 kg (9,914 lb)
Dry mass2,253 kg (4,967 lb)
Start of mission
Launch date4 May 2007, 22:29 UTC
Rocket Ariane 5ECA (V176)
Launch site Centre Spatial Guyanais, ELA-3
Contractor Arianespace
Entered serviceJuly 2007
Orbital parameters
Reference system Geocentric orbit [2]
Regime Geostationary orbit
Longitude19.2° East
Transponders
Band31 transponders:
29 Ku-band
2 Ka-band
Coverage areaEurope
←  Astra 1KR
Astra 1M →
 

Astra 1L, is one of the Astra geostationary satellites owned and operated by SES, was purchased in June 2003.

Launch

It was launched on 4 May 2007, at 22:29 UTC by an Ariane 5ECA from Centre Spatial Guyanais at Kourou, French Guiana. [3]

Satellite description

The satellite is based on the A2100AXS satellite bus, manufactured by Lockheed Martin Commercial Space Systems, Newtown, Pennsylvania, and has a minimum service life of 15 years. [1] It features 29 Ku-band and 2 Ka-band transponders to service Europe. [4] SES stated that Astra 1L would replace Astra 2C. [5]

See also

References

  1. ^ a b "Astra 1L". Gunter's Space page. 21 July 2019. Retrieved 9 April 2021.
  2. ^ "ASTRA 1L". N2YO.com. Retrieved 9 April 2021.
  3. ^ "Display: Astra 1L 2007-016A". nssdc.gsfc.nasa.gov. NASA. 5 April 2021. Retrieved 9 April 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  4. ^ "Satellites". SatBeams. Retrieved 9 April 2021.
  5. ^ "SES ASTRA PROCURES TWO SATELLITES WITH LOCKHEED MARTIN" (Press release). SES Astra. 17 June 2003. Retrieved 26 January 2012.


From Wikipedia, the free encyclopedia

Astra 1L
Mission type Communications
Operator SES
COSPAR ID 2007-016A Edit this at Wikidata
SATCAT no.31306
Website https://www.ses.com/
Mission duration15 years (planned)
16 years, 11 months, 23 days (elapsed)
Spacecraft properties
Spacecraft type Lockheed Martin A2100 [1]
Bus A2100AXS
Manufacturer Lockheed Martin
Launch mass4,497 kg (9,914 lb)
Dry mass2,253 kg (4,967 lb)
Start of mission
Launch date4 May 2007, 22:29 UTC
Rocket Ariane 5ECA (V176)
Launch site Centre Spatial Guyanais, ELA-3
Contractor Arianespace
Entered serviceJuly 2007
Orbital parameters
Reference system Geocentric orbit [2]
Regime Geostationary orbit
Longitude19.2° East
Transponders
Band31 transponders:
29 Ku-band
2 Ka-band
Coverage areaEurope
←  Astra 1KR
Astra 1M →
 

Astra 1L, is one of the Astra geostationary satellites owned and operated by SES, was purchased in June 2003.

Launch

It was launched on 4 May 2007, at 22:29 UTC by an Ariane 5ECA from Centre Spatial Guyanais at Kourou, French Guiana. [3]

Satellite description

The satellite is based on the A2100AXS satellite bus, manufactured by Lockheed Martin Commercial Space Systems, Newtown, Pennsylvania, and has a minimum service life of 15 years. [1] It features 29 Ku-band and 2 Ka-band transponders to service Europe. [4] SES stated that Astra 1L would replace Astra 2C. [5]

See also

References

  1. ^ a b "Astra 1L". Gunter's Space page. 21 July 2019. Retrieved 9 April 2021.
  2. ^ "ASTRA 1L". N2YO.com. Retrieved 9 April 2021.
  3. ^ "Display: Astra 1L 2007-016A". nssdc.gsfc.nasa.gov. NASA. 5 April 2021. Retrieved 9 April 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  4. ^ "Satellites". SatBeams. Retrieved 9 April 2021.
  5. ^ "SES ASTRA PROCURES TWO SATELLITES WITH LOCKHEED MARTIN" (Press release). SES Astra. 17 June 2003. Retrieved 26 January 2012.



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