Official name COSMOS 2517 (GEO-IK)
Alternative name Cosmos-2517 (Geo-IK-2-2)
Cospar ID 2016-034A
Norad ID 41579
Launch date 2016-06-04
Launch site PKMTR
Launch vehicle Rokot-KM
Country/Organization Russia
Type application Geodesy
RCS size LARGE
Decay date ON ORBIT
Period (min) 103.9
Inclination (deg) 99.19
Perigee (km) 942
Apogee (km) 944
Eccentricity 0.00106044538706257
Mean motion (revs. per day) 13.8594802694899
Semi-Major axis (km) 7321.135
Raan (deg) 156.9853
Arg of perigee (deg) 97.9804
Shape Cyl + 2 Pan
Mass (kg) 900
Diameter (m) 1.3
Height (m) 3
Span (m^2) 3
Contractors ISS Reshetnev (ex NPO Prikladnoi Mekhaniki, NPO PM) (prime), Thales Alenia (altimeter)
Equipment SADKO radar altimeter, Laser retro reflectors, GLONASS and GPS receiver
Configuration 3-Axis stabilized Uragan-M bus ?
Power 2 deployable solar arrays, batteries

The Geo-IK-2 is a follow on geodesy mission to the GEO-IK series.

The GEO-IK-2 satellite is the basic element of the similarly-named geodetic satellite system intended for performing geodetic analyses. For instance, the GEO-IK system allows determination of the Earth?s gravitational field parameters; creation of high-accuracy geodetic networks in the geocentric coordinate system; observations of the continental plateaus movement, tides and the Earth?s rotation speed. Besides, with the help of the GEO-IK system position coordinates of ground points can be determined with high accuracy, which is crucial for regional geodetic networks, remote sensing of the Earth, determination of the geoid and monitoring of the ice conditions

The satellite consists of a pressurized container, that is 1.3 m in diameter and length, heat-regulation shutters, honeycomb panels (with a radiator), and an astroplate with an antenna assembly and rigidly fixed solar arrays. The satellite is unified with other spacecraft manufactured by the JSC ISS. The satellite unification speeded up the process of its development. In particular, some elements of the electric power supply system and the thruster units of the propulsion system were taken from the Uragan-M (GLONASS-M)M spacecraft, parts of the attitude and orbit control system were borrowed from SESAT, Ekspress-AM and Luch-4.

The Geo-IK-2 satellites feature following instruments:

  • SADKO radar altimeter built by Thales Alenia
  • Laser retro reflectors
  • GLONASS and GPS receiver

The GEO-IK-2 system consists of two spacecraft to perform geodetic measurements and determine orbit characteristics. The satellites are put into a 1000 km orbit by Rokot-KM or alternatively by Soyuz-2-1v Volga or Angara-1.2 rockets launched at the Plesetsk cosmodrome.

The first launch on board of a Rokot-KM booster took place on 1 February 2011. The launch failed to reach the correct orbit and ground controllers were initially not able to establish contact with the satellite called Kosmos 2470. After evaluations to use the satellite from this orbit, it was finally declared a total loss in June 2011. It reentered on July 15,2013.

The second satellite was ordered to be launched in 2014, but the launch has slipped until 2016.

In August 2012, a third satellite was ordered as a replacement for the lost mission. It was planned to be launched in 2018, but was launched in August 2019.

Satellite COSPAR Date LS Launch Vehicle Remarks
GEO IK 2 2011-005A 2011-02-01 PKMTR Rokot-KM
COSMOS 2517 (GEO-IK) 2016-034A 2016-06-04 PKMTR Rokot-KM
COSMOS 2540 2019-057A 2019-08-30 PKMTR Rokot-KM