| 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. |