COSMOS 1939 (Kosmos-1939) is an Earth observation satellite identified by NORAD_CAT_ID as 19045 and OBJECT_ID as 1988-032A. It was launched on April 20, 1988, from the Tyuratam Space Center (TYMSC), Launch Pad LC31, using a Vostok 8A92M launch vehicle. The satellite uses the SP-1 bus and has dimensions of 6.4 meters in length, 1.4 meters in diameter, and a span of 11.6 meters when its solar arrays are deployed. Its dry mass is 1,900 kilograms, which matches its launch mass. COSMOS 1939 is equipped with MSU-E (2), MSU-SK, and MSU-S instruments for Earth observation purposes. It was manufactured by VNIEM under the Resurs-O program and operated by PRIR. The satellite's power system consists of two deployable solar arrays and batteries. Its shape is described as cylindrical with two panels, and it has a radar cross section (RCS) of 5.612 square meters.