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. |