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CSO 2



General


Designation 47305 / 20104A
Launch date 29 Dec 2020
Country of origin France
Mission Military: Remote sensing (identification)
Perigee/Apogee 480 km, sun-synchronous
Inclination 97.3°
Period  
Launch vehicle Soyuz VS25

same payload as CSO 1

sat-index articles



Technical data



Specifications


Prime contractor Airbus Defence and Space
Platform Astrosat-1000
Mass at launch 3562 kg
Dry mass  
Dimension  
Solar array  
Stabilization 3-axis
DC power  
Design lifetime 10 years


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