 A Progress-M spacecraft | |
| Mission type | Mir resupply |
|---|---|
| COSPAR ID | 1994-075A |
| SATCAT no. | 233481 |
| Spacecraft properties | |
| Spacecraft | Progress (No.225) |
| Spacecraft type | Progress-M2 |
| Manufacturer | RKK Energia |
| Start of mission | |
| Launch date | 11 November 1994, 07:21:58 UTC1 |
| Rocket | Soyuz-U2 |
| Launch site | Baikonur, Site 1/5 |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 16 February 1995, 16:45 UTC3 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 184 km4 |
| Apogee altitude | 238 km4 |
| Inclination | 51.6°4 |
| Period | 88.7 minutes4 |
| Epoch | 11 November 1994 |
| Docking with Mir | |
| Docking port | Kvant-1 aft4 |
| 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
Progress M-25 launched on 11 November 1994 from the Baikonur Cosmodrome in Kazakhstan. It used a Soyuz-U rocket.25
Docking
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.34
Decay
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.34
References
References
- "Launchlog". Jonathan's Space Report. Retrieved 2 December 2020.
- "Progress-M 1 - 13, 15 - 37, 39 - 67 (11F615A55, 7KTGM)". Gunter's Space Page. Retrieved 2 December 2020.
- "Mir". Astronautix. Archived from the original on 20 August 2016. Retrieved 2 December 2020.
- "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. This article incorporates text from this source, which is in the public domain.