 A Progress-M spacecraft | |
| Mission type | Mir resupply |
|---|---|
| COSPAR ID | 1993-052A |
| SATCAT no. | 227451 |
| Spacecraft properties | |
| Spacecraft | Progress (No.219) |
| Spacecraft type | Progress-M2 |
| Manufacturer | RKK Energia |
| Start of mission | |
| Launch date | 10 August 1993, 22:23:45 UTC1 |
| Rocket | Soyuz-U2 |
| Launch site | Baikonur, Site 1/5 |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 19 October 1993, 00:22:14 UTC3 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 179 km4 |
| Apogee altitude | 223 km4 |
| Inclination | 51.8°4 |
| Period | 88.5 minutes4 |
| Epoch | 13 August 1993 |
| Docking with Mir | |
| Docking port | Kvant aft4 |
| Docking date | 13 August 1993, 00:00:06 UTC |
| Undocking date | 12 October 1993, 17:59:06 UTC |
Progress M-19 (Russian: Прогресс M-19) was a Russian unmanned Progress cargo spacecraft, which was launched in 1993 to resupply the Mir space station.
Launch
Progress M-19 launched on 10 August 1993 from the Baikonur Cosmodrome in Kazakhstan. It used a Soyuz-U rocket.2
Docking
Progress M-19 docked with the aft port of the Kvant-1 module of Mir on 13 August 1993 at 00:00:06 UTC, and was undocked on 12 October 1993 at 17:59:06.4
Decay
It remained in orbit until 18 October 1993, when it was deorbited. The mission ending occurred at 00:22:14 UTC on 19 October 1993, when the VBK-Raduga 8 capsule landed.3
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-19"". Manned Astronautics figures and facts. Archived from the original on 9 October 2007.