SOYUZ-TMA 9, also known as Soyuz TMA-9, is a crewed spacecraft manufactured by RKKE and launched on September 18, 2006, from the Tyuratam Site (TYMSC) Launch Complex 1 (LC1), using the Soyuz-FG launch vehicle. It has dimensions of 7.9 meters in length, with a diameter of 2.7 meters and a span of 10.6 meters. The spacecraft has a dry mass of 2300 kg and was launched with a mass of 2877 kg. Its configuration consists of a cylinder, cone, sphere, and two panels, powered by two deployable fixed solar arrays and batteries. It is equipped with Soyuz 11F732 No. 219 payload and serves the purpose of crewed spacecraft missions. The satellite's orbital stability was confirmed on September 18, 2006, at 04:17 UTC.