Astra 2G

from Wikipedia, the free encyclopedia
Astra 2G
Start date December 27, 2014, 21:37 ( UTC )
Launcher Proton-M / Bris-M
Launch site Baikonur
COSPAR-ID : 2014-089A
Takeoff mass 6002 ± 20 kg
Span in orbit 31 m
Manufacturer EADS Astrium
Satellite bus Eurostar E3000
lifespan 15 years
Stabilization three-axis stabilized
operator SES
Playback information
Transponder 62 Ku-band and 4 Ka-band transponders
Bandwidth Ka-band: 250 & 500 & 600 MHz
Others
Electrical power 13 kW
position
First position 28.2 ° East
List of geostationary satellites

Astra 2G is a commercial communications satellite of SES Global based in Betzdorf in Luxembourg .

The satellite was launched into geostationary orbit from the Baikonur rocket launch site on December 27, 2014 at 21:37 UTC with a Proton M / Bris-M launcher .

Since 2015, Astra 2G has made capacities available to Eutelsat , which are marketed under the satellite name Eutelsat 28G.

The three-axis stabilized satellite is equipped with 62 Ku-band and 4 Ka-band transponders and is intended to provide radio and broadband services from a position of 28.2 ° East from Europe, the Middle East and Africa. It was based on the satellite bus built Euro E3000 EADS Astrium and has a design life of 15 years.Template: future / in 5 years

Web links

Individual evidence

  1. Spaceflight101: Astra 2G - Proton Launch Updates - Spaceflight101 ( Memento from February 6, 2015 in the Internet Archive ), accessed on February 8, 2015
  2. a b c SatBeams: Satellite Details - Astra 2G , accessed on February 8, 2015
  3. Full Year 2014–15 RESULTS. Eutelsat, accessed August 17, 2017 .