SOYUZ-TMA 13 (also known as Soyuz TMA-13) is a crewed spacecraft manufactured by RKKE and launched on October 12, 2008, from the Tyuratam Space Center (TYMSC), LC1 launch pad using a Soyuz-FG launch vehicle. The spacecraft has dimensions of 7.9 meters in length, with a diameter of 2.7 meters, and spans 10.6 meters when deployed. It had a launch mass of 2,917 kg and a dry mass of 2,850 kg. SOYUZ-TMA 13 was powered by two deployable fixed solar arrays and batteries, and its shape consists of a cylinder, cone, sphere, and two panels (Cyl + Cone + Sphere + 2 Pan). The satellite is categorized under the BUS type 7K-STMA with no additional equipment noted. Its mission was to transport crew members to the International Space Station.