
Polyot 2 (I1P)
Polyot 2 (I1) was a mission to test the propulsion of the I2P coorbital ASAT satellite. It did not conduct any interception maneuveres.
| Nation: | USSR |
|---|---|
| Type / Application: | ASAT technology |
| Operator: | |
| Contractors: | |
| Equipment: | |
| Configuration: | |
| Propulsion: | |
| Power: | Batteries |
| Lifetime: | |
| Mass: | |
| Orbit: | 303 km × 472 km, 58.06� |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| Polyot 2 (I1P #1) | 1964-019A | 12.04.1964 | Ba LC-31/6 | 11A59 I1P |
