 A Progress-M spacecraft | |
| Mission type | Mir resupply |
|---|---|
| COSPAR ID | 1995-005A |
| SATCAT no. | 23477[1] |
| Spacecraft properties | |
| Spacecraft | Progress (No.226) |
| Spacecraft type | Progress-M[2] |
| Manufacturer | RKK Energia |
| Start of mission | |
| Launch date | 15 February 1995, 16:48:28 UTC[1] |
| Rocket | Soyuz-U[2] |
| Launch site | Baikonur, Site 1/5 |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 15 March 1995, 06:15 UTC[3] |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 188 km[4] |
| Apogee altitude | 224 km[4] |
| Inclination | 51.6°[4] |
| Period | 88.6 minutes[4] |
| Epoch | 15 February 1995 |
| Docking with Mir | |
| Docking port | Kvant-1 aft[4] |
| Docking date | 17 February 1995, 18:21:34 UTC |
| Undocking date | 15 March 1995, 02:26:38 UTC |
Progress M-26 (Russian: Прогресс M-26) was a Russian unmanned Progress cargo spacecraft, which was launched in February 1995 to resupply the Mir space station.
- ^ a b "Launchlog". Jonathan's Space Report. Retrieved 2 December 2020.
- ^ a b "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.
- ^ a b c d e "Cargo spacecraft "Progress M-26"". Manned Astronautics figures and facts. Archived from the original on 9 October 2007.