Satellite Raduga 1-M2 (Raduga 1-9) of Ministry of Defense

Name of Satellite, Alternate Names Raduga 1-M2 (Raduga 1-9)
Country of Operator/Owner Russia
Operator/Owner Ministry of Defense
Users Military
Purpose Communications
Class of Orbit GEO
Type of Orbit
Longitude of GEO (degrees) 70
Perigee (km) 35784
Apogee (km) 35788
Eccentricity 4.74428313881772E-05
Inclination (degrees) 0.01
Period (minutes) 1436.06
Launch Mass (kg.) 2500
Dry Mass (kg.)
Power (watts)
Date of Launch 28-01-2010
Expected Lifetime 5 yrs.
Contractor Applied Mechanics (NPO)
Country of Contractor Russia
Launch Site Baikonur Cosmodrome
Launch Vehicle Proton M
COSPAR Number 2010-002A
NORAD Number 36358
Comments Military communication.


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