Overview
Most satellites constructed by EADS Astrium are launched for commercial use (54.5%) and for the purpose of communications (65.9%).Majority of these satellites are GEO satellites, with around 29 (65.9%) launched so far.
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Insights from the dataset of satellites constructed by EADS Astrium
Which year saw the most satellites launched?
Who operates or owns the most satellites constructed by EADS Astrium?
Which country operates or owns the most satellites constructed by EADS Astrium?
Which rocket has delivered the most satellites constructed by EADS Astrium to space?
Which launch site has launched the most satellites constructed by EADS Astrium to space?
What is the most common type of satellite orbit?
Apogee, Perigee & Period
Satellite Mass
Highlights on some of the satellites constructed by EADS Astrium:
Operated by SES S.A. of Luxembourg, Astra 2F is a commercial satellite launched for the purpose of communications.
A GEO satellite, it was launched into space using Ariane 5 ECA as the launch vehicle from Guiana Space Center on 28 September 2012. Astra 2F was constructed by EADS Astrium (France/UK/Germany).
Designed with an operational lifetime of 15 years, Astra 2F has a launch mass of 6,000 kg and dry mass of 2,660 kg. It navigates with the COSPAR ID 2012-051A and NORAD ID 38778.
Taking 1,436 minutes to orbit the Earth, the satellite's perigee, which is the point of the orbit closest to the Earth's center of mass, is 35,777km while its apogee, which is the point of the orbit farthest from the Earth's center of mass, is 35,795km. The eccentricity of the orbit is 2.13E-04 and it orbits along the Earth longitude of 28 degrees.
Designed for earth observation (Radar Imaging), Cryosat-2 is a government satellite operated by European Space Agency (ESA) (ESA).
Constructed by EADS Astrium (France/UK/Germany/Spain), it was launched into space on 8 April 2010 using Dnepr as the launch vehicle from Baikonur Cosmodrome. Cryosat-2 orbits around the Earth as a polar LEO satellite.
Cryosat-2 has a launch mass of 720 kg and is expected to have a operational lifetime of 3 years. It navigates with the COSPAR ID 2010-013A and NORAD ID 36508.
With an orbital eccentricity of 7.76E-04, the satellite's perigee, which is the point of the orbit closest to the Earth's center of mass, is 713km while its apogee, which is the point of the orbit farthest from the Earth's center of mass, is 724km. It takes 99 minutes to orbit the Earth at an inclination of 92 degrees to the equatorial plane of the Earth.
Heaviest satellite launched by ESA And EUMETSAT (European Organization For The Exploitation Of Meterological Satellites) into space at 4,193 kg
Operated by ESA and EUMETSAT (European Organization for the Exploitation of Meterological Satellites) of Multinational, MetOp-A is a government and civil satellite launched for the purpose of earth observation (Earth Science and Meterology).
A sun-synchronous LEO satellite, it was launched into space using Soyuz-Fregat(Soyuz-2) as the launch vehicle from Baikonur Cosmodrome on 19 October 2006. MetOp-A was constructed by EADS Astrium (France/UK/Germany/Spain).
Designed with an operational lifetime of 5 years, MetOp-A has a launch mass of 4,193 kg and dry mass of 3,750 kg. It navigates with the COSPAR ID 2006-044A and NORAD ID 29499.
Taking 101 minutes to orbit the Earth, the satellite's perigee, which is the point of the orbit closest to the Earth's center of mass, is 820km while its apogee, which is the point of the orbit farthest from the Earth's center of mass, is 821km. The eccentricity of the orbit is 6.95E-05 and it orbits at an inclination of 99 degrees to the equatorial plane of the Earth.
Get more insights from these satellite datasets
Full datasets: All satellites by launch date | The Heaviest Satellites That Are Launched to Space
By Use Type: Civil-use satellites | Commercial satellites | Government satellites | Military satellites
By Country: USA | UK | France | Germany | Japan | China | Russia | Australia | Canada
By Orbit Class/Type: LEO satellites | MEO satellites | GEO satellites | Elliptical orbit | Polar orbit | Equatorial orbit | Non-polar inclined orbit | Sun-synchronous orbit | Molniya orbit
By Operators: SpaceX | EUTELSAT | SES | European Space Agency (ESA) | Planet Labs | Iridium | Spire Global | OneWeb | Swarm Technologies | NASA - Dataset of Satellites Launched (National Aeronautics and Space Administration) | Canadian Space Agency (CSA) - Dataset of Satellites Launched
By Launch Vehicle: Falcon 9 | Ariane 5 | Ariane 5 ECA | Delta 2 | Dnepr | Electron | Falcon Heavy | Long March 2C | Long March 2D | Long March 3B | Pegasus | Proton | Proton M | PSLV | Rokot | Soyuz | Soyuz-2.1b | Vega
By Launch Vehicle: Cape Canaveral | Baikonur Cosmodrome | Guiana Space Center | International Space Station | Jiuquan Satellite Launch Center | Plesetsk Cosmodrome | Rocket Lab Launch Complex 1 | Satish Dhawan Space Centre | Taiyuan Launch Center | Vandenberg AFB | Xichang Satellite Launch Center | Boeing Satellite Systems | Airbus Defense and Space | EADS Astrium | Lockheed Martin Commercial Space Systems | Space Systems/Loral | Surrey Satellite Technology | Technical University Berlin | Thales Alenia Space
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