PROGRESS-M 20 (also known as Progress M-20) is a cargo spacecraft with NORAD ID 22867 and OBJECT_ID 1993-064A, manufactured by NPOE in Russia. Launched on October 11, 1993, from the TYMSC launch site using Soyuz-U as the launch vehicle, it measures 7.9 meters in length and has a diameter of 2.7 meters with a span also at 7.9 meters. The dry mass is recorded as 4500 kg while its launch mass was 7130 kg. Equipped with two deployable fixed solar arrays and batteries for power, the satellite's shape consists of a sphere, cone, cylinder, and pan. It carries a Progress 7K-TGM No. 220 payload designed for cargo missions and uses a KTDU-80 (S5.80) motor. The spacecraft has an RCS (Reaction Control System) capacity of 18.5 kg.