The Kondor-FKA is a small civilian radar Earth observation satellite designed by NPO Mashinostroyeniya as a civilian counterpart to the Kondor-E satellite. The Kondor satellite features a S-band synthetic aperture radar (SAR), which can conduct both continous swath surweys or detailed spot surveys. The swath width is 10 km. Ground resolution is 1 to 2 m in spotlight mode, 1 to 3 m in stripmap mode and 5 to 30 m in ScanSAR mode.
Sun-Synchronous OrbitGlonass-K2 are the fourth generation of satellite design for GLONASS satellite navigation system. GLONASS is a Russian space-based navigation system comparable to the similar GPS and Galileo systems. This generation improves on accuracy, power consumption and design life. Each satellite is unpressurized and weighs 1645 kg, and has an operational lifetime of 10 years.
Medium Earth OrbitGlonass-K are the third generation of satellite design for GLONASS satellite navigation system. GLONASS is a Russian space-based navigation system comparable to the similar GPS and Galileo systems. This generation improves on accuracy, power consumption and design life. Each satellite is unpressurized and weighs 935 kg, and has an operational lifetime of 10 years.
Medium Earth OrbitGlonass-K are the third generation of satellite design for GLONASS satellite navigation system. GLONASS is a Russian space-based navigation system comparable to the similar GPS and Galileo systems. This generation improves on accuracy, power consumption and design life. Each satellite is unpressurized and weighs 935 kg, and has an operational lifetime of 10 years.
Medium Earth OrbitA pair of Russian optical Earth observation satellites built by the Progress Rocket Space Centre for obtaining stereo images of the Earth's surface, with maximum resolution of 1.2 m in panchromatic mode and a swath width of 32 km.
Sun-Synchronous OrbitThe Russian Obzor-R satellite is a planned X-band radar earth observation satellite designed by TsSKB-Progress. In 2012, the development of the Arkon-2M radar satellite was stopped and instead the development of the Obzor-R was initiated. The satellite features the BRLK X-band Synthetic Aperture Radar as the imaging instrument with a ground resolution of 500 m.
Sun-Synchronous OrbitLuna 26 (also named Luna-Resurs) is a planned lunar polar orbiter, part of the Luna-Glob program, by the Russian space agency Roscosmos. In addition to its scientific role, the Luna 26 orbiter would also function as a telecommunication relay between Earth and Russian landed assets. The scientific payload on board the orbiter is composed of fourteen instruments that will be fabricated by Russia. The payload will study the lunar surface and the environment around the Moon, including the solar wind, and high-energy cosmic rays. Luna 26 will also scout sites for the planned Luna 27 landing mission. Luna 26 is the second mission of Russia's new lunar program, which includes the launch of Luna 27, a heavy lander that will study the composition of the lunar soil by collecting several samples. Luna 28, a lunar samples return mission, will be the first to return samples at lunar temperature, and will serve as a demonstration for a future Martian samples return mission. Finally, Luna 29 should land a heavy lunar rover on the surface.
Lunar OrbitLuna 27 (also named Luna-Resurs 1) is a planned lunar lander mission by Roscosmos to send a lander to the South Pole–Aitken basin, an area on the far side of the Moon. The purpose is to prospect for minerals, volatiles (nitrogen, water, carbon dioxide, ammonia, hydrogen, methane and sulfur dioxide, and lunar water ice in permanently shadowed areas of the Moon and investigate the potential use of these natural lunar resources. On the long term, Russia considers building a crewed base on the Moon's far side that would bring scientific and commercial benefits. The lander will feature 15 science instruments that will analyse the regolith, plasma in the exosphere, dust, and seismic activity. The payload will include a sampling drill.
Lunar Orbit