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| Specification | Proton-M Khrunichev State Research and Production Space Center × remove |
|---|---|
| Flights | 1 |
| Success rate | 100% |
| Thrust | 10,532 kN |
| Height | 58.2 m |
| Diameter | 7.4 m |
| Launch mass | 705 t |
| LEO capacity | 23,000 kg |
| GTO capacity | 6,920 kg |
| Launch cost | $65M |
| Reusable | No |
| Stages | 3 |