SOYUZ-TMA 10M (Soyuz TMA-10M) is a crewed spacecraft launched on September 25, 2013, from the Tyuratam Space Center Launch Site LC1 using a Soyuz-FG launch vehicle. Manufactured by RKKE, this spacecraft measures 7.9 meters in length and has a diameter of 2.7 meters with a span of 10.6 meters. It weighs 2900 kg both at launch and dry mass. The mission's payload is the Soyuz 11F732A47 No. 710, designed for crew transportation. Equipped with two deployable fixed solar arrays and batteries, it serves as a cylindrical spacecraft topped by a cone, sphere, and two panels.