Astra 1L

Astra 1L
Mission typeCommunications
OperatorSES
COSPAR ID2007-016A Edit this at Wikidata
SATCAT no.31306
Websitehttps://www.ses.com/
Mission duration15 years (planned)
17 years, 6 months, 19 days (elapsed)
Spacecraft properties
Spacecraft typeLockheed Martin A2100[1]
BusA2100AXS
ManufacturerLockheed 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
RocketAriane 5ECA (V176)
Launch siteCentre Spatial Guyanais, ELA-3
ContractorArianespace
Entered serviceJuly 2007
Orbital parameters
Reference systemGeocentric orbit[2]
RegimeGeostationary orbit
Longitude19.2° East
Transponders
Band31 transponders:
29 Ku-band
2 Ka-band
Coverage areaEurope

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

  1. ^ Cite error: The named reference Gunter was invoked but never defined (see the help page).
  2. ^ "ASTRA 1L". N2YO.com. Retrieved 9 April 2021.