IRIDIUM 20 (also known as Iridium 20A) is a communication satellite with NORAD Catalog ID 25577 and OBJECT_ID 1998-074A, manufactured by MOTO under the LM700 BUS configuration. Launched on December 19, 1998, from Taiyuan Satellite Launch Center (TAISC) using a Chang Zheng 2C-III/SD launch vehicle, it has dimensions of 3.5 meters in length and 1 meter in diameter with a span of 5 meters. The satellite's dry mass is 556 kg, and its launch mass was 667 kg. It uses two deployable solar arrays and batteries for power generation. The satellite's shape is described as Box + 2 Pan with an RCS of 3.6949 m². Its mission is to provide communication services, operating in a low Earth orbit with an expected lifetime of 8 years.