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Astra 1M

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Astra 1M
Mission type Communications
Operator SES
COSPAR ID 2008-057A Edit this at Wikidata
SATCAT no. 33436
Website https://www.ses.com
Mission duration 15 years (planned)
15 years, 6 months, 18 days (elapsed)
Spacecraft properties
Spacecraft type Eurostar
Bus Eurostar 3000S
Manufacturer Astrium
(now Airbus Defence and Space )
Launch mass 5,320 kg (11,730 lb)
Power 10 kW
Start of mission
Launch date 5 November 2008, 20:44:20 UTC
Rocket Proton-M / Briz-M
Launch site Baikonur , Site 200/39
Contractor Khrunichev State Research and Production Space Center
Entered service January 2009
Orbital parameters
Reference system Geocentric orbit
Regime Geostationary orbit
Longitude 19.2° East
Transponders
Band 36 Ku-band
Bandwidth 26 MHz
33 MHz
Coverage area Europe, Africa, Middle East
←  Astra 1L
Astra 3B  →
 

Astra 1M is a geostationary communications satellite which is operated by SES . It is positioned in geostationary orbit at a longitude of 19.2° East , from where it is used to provide direct to home (DTH) broadcasting to Europe, Africa , and the Middle East .

Satellite description [ edit ]

Astra 1M was built by Astrium (now Airbus Defence and Space ) under a contract signed in July 2005, and is based on the Eurostar 3000S satellite bus . It is equipped with thirty six transponders operating in the J-band of the NATO-defined spectrum, or the Ku-band of the older IEEE -defined spectrum. At launch it had a mass of 5,320 kg (11,730 lb), [1] with an expected operational lifespan of 15 years, [2] however four of its transponders were deactivated five years after launch. [3] At the beginning of its operational life, it had a maximum power consumption of 10 kilowatts by the end of the satellite's operational life. [3]

Launch [ edit ]

The launch of Astra 1M was conducted by International Launch Services (ILS), using a Proton-M launch vehicle with a Briz-M upper stage. The launch occurred from Site 200/39 at the Baikonur Cosmodrome in Kazakhstan , at 20:44:20 UTC on 5 November 2008. [4] Astra 1M was successfully placed into a geostationary transfer orbit (GTO), from which it raised itself to geostationary orbit by means of an onboard apogee motor .

See also [ edit ]

References [ edit ]

  1. ^ "Astra 1M" . SES Astra . Retrieved 10 April 2021 .
  2. ^ "UCS Satellite Database" . Union of Concerned Scientists. 1 April 2010. Archived from the original on 3 June 2010 . Retrieved 31 May 2010 .
  3. ^ a b "Astra 1M" . Gunter's Space Page. 11 December 2017 . Retrieved 10 April 2021 .
  4. ^ McDowell, Jonathan (14 March 2021). "Launch Log" . Jonathan's Space Report . Retrieved 10 April 2021 .

External links [ edit ]