Facts and figures
Full name: CryoSat
Instrument: SAR Interferometric Radar Altimeter (SIRAL), supported by Doppler Orbit and Radio Positioning Integration by Satellite (DORIS) and Laser Retro-Reflector (LRR) for precision orbit determination
Mass: 720 kg at launch, including 37 kg of fuel
Power: 2 × GaAs body-mounted solar arrays, each delivering 850 W; 78 Ah Li-ion battery
Launched: 8 April 2010
Launch site: Baikonur Cosmodrome, Kazakhstan
Launcher: Russian/Ukrainian Dnepr based on SS-18 intercontinental ballistic missile
Launch provider: International Space Company Kosmotras
Orbit: Mean altitude of 717 km and inclination of 92°; low Earth, polar, non-Sun-synchronous
Mission control: ESA’s European Satellite Operations Centre (ESOC) in Darmstadt, Germany
Ground station: Science data downloaded to ESA’s ground station in Kiruna, Sweden
Data processing: Data distributed directly to users from the ground station in Kiruna, Sweden; distribution and mission planning managed via ESA’s Centre for Earth Observation (ESRIN) in Frascati, Italy; long-term archive at a dedicated facility at the Centre National d’Etudes Spatiales (CNES) in Toulouse, France
Nominal life: three years (including a six-month commissioning phase) with a possible two-year extension
Satellite Prime Contractor: EADS Astrium
- ESRIN
http://www.esa.int/About_Us/ESRIN - Operations
http://www.esa.int/Our_Activities/Operations - Kiruna station
http://www.esa.int/Our_Activities/Operations/Kiruna_station - Baikonur Cosmodrome
http://www.kosmotras.ru/en/bayconur/ - Kosmotras
http://www.kosmotras.ru/en/ - EADS Astrium
http://www.astrium.eads.net - CNES
http://www.cnes.fr/web/CNES-en/455-cnes-en.php - DORIS
http://www.cnes.fr/web/CNES-en/1513-doris.php - SIRAL
http://www.thalesgroup.com/Case_Studies/CaseStudy_space_SIRAL/?pid=1576 - Fact sheet
http://esamultimedia.esa.int/docs/Cryosat/Cryosat-Factsheet-22-March-2010.pdf - Fact sheet (German)
http://esamultimedia.esa.int/docs/Cryosat/Cryosat-Factsheet-Deutsch-22-March-2010.pdf
