Yantar-2K ( meaning amber) was a type of Soviet reconnaissance satellite which supplemented and eventually replaced the Zenit spacecraft. It was the first satellite of the Yantar series and was managed by the Soviet military intelligence agency, the GRU. These satellites were in orbit for 30 days and photographed sites of interest using a film camera. Yantar-2K was proposed in 1967 and had its first test launch in May 1974. It was in military service from 1978 to 1983 and was given the name Feniks (), meaning phoenix. Equipment Yantar differed from Zenit in that it had to stay in orbit for a month unlike Zenit's 8–14 days. It also had 2 film return capsules, something it had in common with the US KH-7 GAMBIT reconnaissance satellite. Yantar had three parts: the aggregate/equipment module (AO - Agregatnyy Otsek), the instrument module (PO - Pribornnyy Otsek) and the special equipment module/special apparatus module (OSA - otsek spetsialnoy apparatury). The special equipment module was the part that returned to earth at the end of the mission, and contained the Zhemchug-4 (pearl) camera. Each section was shaped like a truncated cone which gave the craft a conical shape. The craft was 6.3m long (although one source says 8.5m) with a maximum diameter of 2.7m. It weighed 6.6 tonnes. The aggregate module was 1.2m long and 2.7m diameter and contained the propulsion unit. It used UDMH fuel with an oxidiser. Attached to it were two solar arrays, each six metres long with four panels. The instrument module was 1m long and 2.4m diameter. It contained most of the equipment including Kvadrat gyroscopes, telemetry systems and attitude control. It was covered in thermal radiator panels. The special equipment module was 3.3m long with a diameter of 2.3m. A shade 2.5m long with a diameter of 0.9m was attached to the front. The module contained the Zhemchug-4 camera, the Salyut-3M computer, film and film handling systems. It also acted as the reentry vehicle. Attached to it were two film return capsules (SpK Spuskayemaya Kapsula) which were 0.8m diameter spheres. They contained retro rockets and could land on the ground or on water. During a thirty-day mission the film return capsules deorbited on the tenth and eighteenth days with the final film returning with the re-entry vehicle. Space historian Peter Gorin estimates that the camera lens had a diameter of 600mm and a focal length of approximately