 A Progress 7K-TG spacecraft | |
| Mission type | Mir resupply |
|---|---|
| COSPAR ID | 1986-023A |
| SATCAT no. | 16645[1] |
| Spacecraft properties | |
| Spacecraft | Progress (No.134) |
| Spacecraft type | Progress 7K-TG[2] |
| Manufacturer | NPO Energia |
| Start of mission | |
| Launch date | 19 March 1986, 10:08:25 UTC[1] |
| Rocket | Soyuz-U2[2] |
| Launch site | Baikonur, Site 1/5 |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 21 April 1986, 00:00 UTC[3] |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 183 km[3] |
| Apogee altitude | 251 km[3] |
| Inclination | 51.7°[3] |
| Period | 88.8 minutes[3] |
| Epoch | 19 March 1986 |
| Docking with Mir | |
| Docking port | Mir Core Module aft[3] |
| Docking date | 21 March 1986, 11:16:02 UTC |
| 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.
- ^ a b "Launchlog". Jonathan's Space Report. Retrieved 5 December 2020.
- ^ a b "Progress 1 - 42 (11F615A15, 7K-TG)". Gunter's Space Page. Retrieved 5 December 2020.
- ^ a b c d e f "Cargo spacecraft "Progress 25"". Manned Astronautics figures and facts. Archived from the original on 9 October 2007.