COSMOS 2120 (also known as Kosmos-2120) is a reconnaissance satellite launched on December 26, 1990, from the Plesetsk Cosmodrome's LC16/2 launch pad using the Soyuz-U-PVB launch vehicle. The satellite was manufactured by TSSKB and belongs to the SU (Soviet Union). It has a configuration known as Zenit bus and is based on the Oblik platform. Its dimensions include a length of 6 meters, diameter of 2.2 meters, and span of 6 meters. The dry mass and launch mass are both recorded at 2655 kg. The satellite is powered by batteries and its mission involves reconnaissance with film return capability. It features a Sphere + DCone shape design and uses the 11D82M; S5.120 maneuver module for propulsion.