A Progress-M spacecraft | |
Mission type | Mir resupply |
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COSPAR ID | 1995-036A |
SATCAT no. | 23617 |
Spacecraft properties | |
Spacecraft | Progress (No.228) |
Spacecraft type | Progress-M |
Manufacturer | RKK Energia |
Start of mission | |
Launch date | 20 July 1995, 03:04:41 UTC |
Rocket | Soyuz-U |
Launch site | Baikonur, Site 1/5 |
End of mission | |
Disposal | Deorbited |
Decay date | 4 September 1995, 08:58:55 UTC |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 191 km |
Apogee altitude | 239 km |
Inclination | 51.6° |
Period | 88.5 minutes |
Epoch | 20 July 1995 |
Docking with Mir | |
Docking port | Mir Core Module forward |
Docking date | 22 July 1995, 05:39:37 UTC |
Undocking date | 4 September 1995, 05:09:53 UTC |
Progress (spacecraft)← Progress M-27Progress M-29 → |
Progress M-28 (Russian: Прогресс M-28) was a Russian unmanned Progress cargo spacecraft, which was launched in July 1995 to resupply the Mir space station.
Launch
Progress M-28 launched on 20 July 1995 from the Baikonur Cosmodrome in Kazakhstan. It used a Soyuz-U rocket.
Docking
Progress M-28 docked with the forward port of the Mir Core Module on 22 July 1995 at 05:39:37 UTC, and was undocked on 4 September 1995 at 05:09:53 UTC.
Decay
It remained in orbit until 4 September 1995, when it was deorbited. The mission ended at 08:58:55 UTC.
See also
References
- ^ "Launchlog". Jonathan's Space Report. Retrieved 3 December 2020.
- ^ "Progress-M 1 - 13, 15 - 37, 39 - 67 (11F615A55, 7KTGM)". Gunter's Space Page. Retrieved 3 December 2020.
- ^ "Mir". Astronautix. Archived from the original on 20 August 2016. Retrieved 3 December 2020.
- ^ "Cargo spacecraft "Progress M-28"". Manned Astronautics figures and facts. Archived from the original on 9 October 2007.
- "Progress M-28". NASA. Retrieved 3 December 2020. This article incorporates text from this source, which is in the public domain.
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