| Cospar id | 1986-023A |
|---|---|
| Satcat | 16645[2] |
| Spacecraft | Progress (No.134) |
| Progress 7K-TG[3] | Progress (No.134) |
| Manufacturer | NPO Energia |
| Launch date | 19 March 1986, 10:08:25 UTC[2] |
| Launch rocket | Soyuz-U2[3] |
| Launch site | Baikonur, Site 1/5 |
| Decay date | 21 April 1986, 00:00 UTC[1] |
| Orbit epoch | 19 March 1986 |
| Orbit reference | Geocentric |
| Orbit regime | Low Earth |
| Orbit periapsis | 183 km[1] |
| Orbit apoapsis | 251 km[1] |
| Orbit inclination | 51.7°[1] |
| Orbit period | 88.8 minutes[1] |
| Apsis | gee |
| Programme | Progress (spacecraft) |
| Previous mission | Kosmos 1669 |
| Next mission | Progress 26 |
| Docking target | Mir |
|---|---|
| dock | 21 March 1986, 11:16:02 UTC |
| Docking port | Mir Core Module aft[1] |
| Undocking date | 20 April 1986, 19:24:08 UTC |
Progress 25 (Russian: Прогресс 25) was a Soviet uncrewed Progress cargo spacecraft, which was launched in March 1986 to resupply the Mir space station.
Launch
Progress 25 launched on 19 March 1986 from the Baikonur Cosmodrome in the Kazakh SSR. It used a Soyuz-U2 rocket.[3][4]
Docking
Progress 25 docked with the aft port of the Mir Core Module on 21 March 1986 at 11:16:02 UTC, and was undocked on 20 April 1986 at 19:24:08 UTC.[1][5]
Decay
It remained in orbit until 21 April 1986, when it was deorbited. The deorbit burn occurred at 00:00 UTC and the mission ended at 00:48:30 UTC.[1][5]
See also
References
- ^ "Cargo spacecraft "Progress 25"". Manned Astronautics figures and facts. Archived 9 October 2007 at the Wayback Machine.
- ^ "Launchlog". Jonathan's Space Report. Retrieved 5 December 2020.
- ^ "Progress 1 - 42 (11F615A15, 7K-TG)". Gunter's Space Page. Retrieved 5 December 2020.
- ^ "Progress 25". NASA. Retrieved 5 December 2020.
- ^ "Mir". Astronautix. Archived from the original on 20 August 2016. Retrieved 5 December 2020.