Soyuz TM-1

Soyuz TM-1

Soyuz TM-1
Mission duration 9 days
Spacecraft properties
Spacecraft type Soyuz-TM
Manufacturer NPO Energia
Launch mass 6,450 kilograms (14,220 lb)
Start of mission
Launch date 21 May 1986 (1986-05-21Z) UTC
Rocket Soyuz-U2
Launch site Baikonur 1/5
End of mission
Landing date Did not recognize date. Try slightly modifying the date in the first parameter. UTC
Orbital parameters
Reference system Geocentric
Regime Low Earth
Docking with Mir

Soyuz TM-1 was an unmanned test flight of the Soyuz-TM spacecraft, intended for use in the Mir space station program. This was the maiden flight of the Soyuz-TM spacecraft, intended as the successor to the Soyuz-T spacecraft used in the Salyut program.

Mission parameters

  • Spacecraft: Soyuz-7K-STM
  • Mass: 6450 kg
  • Crew: None
  • Launched: May 21, 1986
  • Landed: May 30, 1986
==References