| Name of Satellite, Alternate Names | Glonass 712 (Glonass M, Cosmos 2413) |
| Country of Operator/Owner | Russia |
| Operator/Owner | Ministry of Defense |
| Users | Military/Commercial |
| Purpose | Navigation/Global Positioning |
| Class of Orbit | MEO |
| Type of Orbit | |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 19134 |
| Apogee (km) | 19141 |
| Eccentricity | 0.000137214544741743 |
| Inclination (degrees) | 64.8 |
| Period (minutes) | 676.1 |
| Launch Mass (kg.) | 1480 |
| Dry Mass (kg.) | |
| Power (watts) | 1600 |
| Date of Launch | 26-12-2004 |
| Expected Lifetime | 7 yrs. |
| Contractor | NPO-PM |
| Country of Contractor | Russia |
| Launch Site | Baikonur Cosmodrome |
| Launch Vehicle | Proton K |
| COSPAR Number | 2004-053B |
| NORAD Number | 28509 |
| Comments | New Glonass-M type; Russia´s version of the GPS system, functions the same; there has been cooperation between the two; much scaled-back constellation |