US-PM (US-PU) |
Russia |
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US-PM |
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US-PM (Upravlenniye Sputnik Passivny Modifikirovanny) (also reported as US-PU) was a solar powered improved EORSAT (Electronic Ocean Reconnaisance Satellite). It used an passive ELINT devices to track naval vessels from space by registering their electronic emmissions.
US-PM was a modified version of the US-P and replaced both the US-P and the nuclear US-A satellites.
It shared the same US bus with its precedessors, which provided maneuvering capabilities to the spacecraft.
The US-PM were placed into a 420 km orbits inclined 65 degrees by the Tsiklon-2
booster. Systems aboard the 3300 kg satellite included the Radio-Technical
Reconnaissance system and systems for electronic camouflage and self-protection.
An engine unit maintained the orbital altitude and made a final deorbit of the
satellite at the end of the mission.
| Satellite | Date | LS | Launcher | Remarks: |
| Cosmos 2238 [US-PM #1] | 31.03.1993 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2244 [US-PM #2] | 28.04.1993 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2258 [US-PM #3] | 07.07.1993 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2264 [US-PM #4] | 17.09.1993 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2293 [US-PM #5] | 02.11.1994 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2313 [US-PM #6] | 08.06.1995 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2326 [US-PM #7] | 20.12.1995 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2335 [US-PM #8] | 11.12.1996 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2347 [US-PM #9] | 09.12.1997 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2367 [US-PM #10] | 26.12.1999 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2383 [US-PM #11] | 21.12.2001 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2405 (US-PM #12) | 28.05.2004 | B, LC-90 | Tsyklon-2 | |
| Cosmos 2421 (US-PM #13) | 25.06.2006 | B, LC-90 | Tsyklon-2 |
| Ref.: #7, #14 - update: 3.08.06 | Home |