Astra 2C

Astra 2C
Mission typeCommunications
OperatorSES
COSPAR ID2001-025A Edit this at Wikidata
SATCAT no.26853
Websitehttps://www.ses.com/
Mission duration15 years (planned)
23 years, 1 month (elapsed)
Spacecraft properties
Spacecraft typeBoeing 601
BusBSS 601 HP
ManufacturerBoeing Satellite Systems
Launch mass3,643 kg (8,031 lb)
Power7.0 kW
Start of mission
Launch date16 June 2001, 01:49:00 UTC
RocketProton-K / DM-03
Launch siteBaikonur, Site 81/23
ContractorKhrunichev State Research and Production Space Center
Entered serviceAugust 2001
Orbital parameters
Reference systemGeocentric orbit[1]
RegimeGeostationary orbit
LongitudeAstra 23.5°E (2018)
60.2° East (2015–2018)
Astra 28.2°E (2014–2015)
Astra 19.2°E (2010–2014)
Astra 31.5°E (2009–2010)
Astra 28.2°E (2007–2009)
Astra 19.2°E (2001–2007)
Transponders
Band32 Ku-band
Bandwidth33 MHz
Coverage areaEurope
 

Astra 2C is one of the Astra communications satellites owned and operated by SES. Designed to join Astra 2A and Astra 2B at the Astra 28.2°E orbital position providing digital television and radio broadcast services to the United Kingdom and Ireland, the satellite was first used after launch in 2001 at 19.2° East for pan-European coverage.

The satellite provides one broadcast beam with horizontal and vertical polarisation, across a single footprint covering the areas of Central and Eastern Europe, Scandinavia, the Iberian Peninsula and Canary Islands.[2]

TV signals can be received with a 50 cm dish across the majority of the British Isles with a 60 cm dish required in the extreme north and west. Astra 2C can also provide backup capacity, substituting for one or more transponders across the 10.70-12.20 GHz broadcast range used by Astra satellites in the Astra 19.2°E and Astra 28.2°E orbital positions.

  1. ^ "ASTRA 2C". N2YO.com. Retrieved 27 May 2018.
  2. ^ "Astra 2C". SES. Archived from the original on 25 January 2012. Retrieved 26 January 2012.

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