Canopus V specifications


Prime contractor NIIEM Federal State Unitary Enterprise, Istra
Platform  
Mass at launch 460-470 kg
Dry mass 108 kg
Dimension  
Solar array 2 wings
Stabilization 3-axis
DC power 250 W
Design lifetime 5 years

SSTL supplies three suites of satellite avionics and software plus system design support, power management and batteries, on board computers and data handling capabilities for satellite subsystems and satellite operations.
Downlink at 8.048 & 8.3815 GHz (122.88 Mbps)

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