SOYUZ-TM 10 was a crewed spacecraft launched on August 1, 1990, from Tsymlyanskaya Space Center using the Soyuz-U2 launch vehicle. The satellite has the OBJECT_ID of 1990-067A and is also known as Soyuz TM-10. It measures 7.2 meters in length with a diameter of 2.2 meters, a span of 10.6 meters, and had both a launch mass and dry mass of 2850 kilograms. The satellite was manufactured by NPOE and is configured as a sphere + cone + cylinder + two panels, powered by two deployable fixed solar arrays along with batteries. Its propulsion system includes the KTDU-80 (S5.80) motor, and it serves as a crewed spacecraft for space missions.