Progress M-25
 A Progress-M spacecraft | |
| Mission type | Mir resupply |
|---|---|
| COSPAR ID | 1994-075A |
| SATCAT no. | 23348[1] |
| Spacecraft properties | |
| Spacecraft | Progress (No.225) |
| Spacecraft type | Progress-M[2] |
| Manufacturer | RKK Energia |
| Start of mission | |
| Launch date | 11 November 1994, 07:21:58 UTC[1] |
| Rocket | Soyuz-U[2] |
| Launch site | Baikonur, Site 1/5 |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 16 February 1995, 16:45 UTC[3] |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 184 km[4] |
| Apogee altitude | 238 km[4] |
| Inclination | 51.6°[4] |
| Period | 88.7 minutes[4] |
| Epoch | 11 November 1994 |
| Docking with Mir | |
| Docking port | Kvant-1 aft[4] |
| Docking date | 13 November 1994, 09:04:29 UTC |
| Undocking date | 16 February 1995, 13:03:00 UTC |
Progress M-25 (Russian: Прогресс M-25) was a Russian unmanned Progress cargo spacecraft, which was launched in November 1994 to resupply the Mir space station.
Launch
[edit]Progress M-25 launched on 11 November 1994 from the Baikonur Cosmodrome in Kazakhstan. It used a Soyuz-U rocket.[2][5]
Docking
[edit]Progress M-25 docked with the aft port of the Kvant-1 module of Mir on 13 November 1994 at 09:04:29 UTC, and was undocked on 16 February 1995 at 13:03:00 UTC.[3][4]
Decay
[edit]It remained in orbit until 16 February 1995, when it was deorbited. The deorbit burn occurred at 16:06:00 UTC and the mission ended at 16:45 UTC.[3][4]
See also
[edit]
References
[edit]- ^ a b "Launchlog". Jonathan's Space Report. Retrieved 2 December 2020.
- ^ a b c "Progress-M 1 - 13, 15 - 37, 39 - 67 (11F615A55, 7KTGM)". Gunter's Space Page. Retrieved 2 December 2020.
- ^ a b c "Mir". Astronautix. Archived from the original on 20 August 2016. Retrieved 2 December 2020.
- ^ a b c d e f g "Cargo spacecraft "Progress M-25"". Manned Astronautics figures and facts. Archived from the original on 9 October 2007.
- ^ "Progress M-25". NASA. Retrieved 2 December 2020.
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