The RESURS F-1M satellite, also known as Resurs F-1M, was launched on September 28, 1999, from the Plesetsk Cosmodrome LC43/4 launch pad using a Soyuz-U-PVB launch vehicle. With an identification number of NORAD_CAT_ID 25929 and OBJECT_ID 1999-054A, this satellite is part of the Resurs-F1 bus series configured with a Vostok / Zenit Capsule design. Manufactured by PROGT, it was designed for Earth Observation missions using film return technology. The satellite measures 6.5 meters in length and diameter, has a span of 6.5 meters, and weighs approximately 2375 kilograms both at launch and dry mass. It is powered by batteries and stabilized after its stable date on September 29, 1999. Its shape is described as a Sphere + DCone with an RCS (Reaction Control System) of 16.93. The mission's purpose involves Earth Observation using film return technology.