 A Progress 7K-TG spacecraft | |
| Mission type | Mir resupply |
|---|---|
| COSPAR ID | 1987-044A |
| SATCATno. | 17999[1] |
| Spacecraft properties | |
| Spacecraft | Progress (No.128) |
| Spacecraft type | Progress 7K-TG[2] |
| Manufacturer | NPO Energia |
| Start of mission | |
| Launch date | 19 May 1987, 04:02:10 UTC[1] |
| Rocket | Soyuz-U2[2] |
| Launch site | Baikonur,Site 1/5 |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 19 July 1987, 05:00:00 UTC[3] |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 341 km[3] |
| Apogee altitude | 365 km[3] |
| Inclination | 51.6°[3] |
| Period | 91.6 minutes[3] |
| Epoch | 19 May 1987 |
| Docking withMir | |
| Docking port | Kvant-1 aft[3] |
| Docking date | 21 May 1987, 05:50:38 UTC |
| Undocking date | 19 July 1987, 00:19:51 UTC |
Progress 30 (Russian:Прогресс 30) was aSoviet uncrewedProgress cargo spacecraft, which was launched in May 1987 to resupply theMir space station.
Progress 30 launched on 19 May 1987 from theBaikonur Cosmodrome in theKazakh SSR. It used aSoyuz-U2 rocket.[2][4]
Progress 30 docked with the aft port of theKvant-1 module of Mir on 21 May 1987 at 05:50:38 UTC, and was undocked on 19 July 1987 at 00:19:51 UTC.[3][5]
It remained in orbit until 19 July 1987, when it was deorbited. The deorbit burn occurred at 05:00:00 UTC and the mission ended at 05:42 UTC.[3][5]
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