Official name RESURS DK-1
Alternative name Resurs DK-1
Cospar ID 2006-021A
Norad ID 29228
Launch date 2006-06-15
Launch site TTMTR
Launch vehicle Soyuz-U
Country/Organization Russia
Type application Earth Observation, cosmic rays
Operator Roskosmos
RCS size LARGE
Decay date ON ORBIT
Period (min) 95.55
Inclination (deg) 69.93
Perigee (km) 544
Apogee (km) 546
Eccentricity 0.0018348623853211
Mean motion (revs. per day) 15.0706436420722
Semi-Major axis (km) 6923.135
Raan (deg) 165.9933
Arg of perigee (deg) 40.2242
Shape Cyl + 2 Pan
Mass (kg) 6570
Diameter (m) 2.7
Height (m) 7.9
Span (m^2) 10
Lifetime 3 years (minimum); 5 years (planned)
Contractors TsSKB-Progress
Equipment Geoton-L1 Multi-spectral imaging payload, PAMELA particle detector, ARINA earthquake experiment
Configuration Yantar bus
Power 2 deployable solar arrays, batteries

The Russian Resurs-DK 1 (46KS) satellite is mainly designed to image and transmit data on information for Earth natural resources study, data on ecology and emergency, sea surface status, ice situation, meteorological conditions in Earth polar regions, as well as to support digital data exchange between ground users. The satellite is continuously oriented towards the Earth in order to fulfill this program of Earth surface observation.

The spacecraft was built by TsSKB Progress in Samara. It is based on the military Yantar-4KS1M (Neman) imaging satellite.

The main sensor of the spacecraft is the Geoton-L1 optoelectronic push-broom imager. Panchromatic resolution at an altitude of 360 km is 0.9 m, at an altitude of 604 km it is 1.5 m. Multispectral resolution is between 1.5 and 2 m.

The additional Russian and Italian 470 kg PAMELA (Payload for AntiMatter Exploration and Light-nuclei Astrophysics) magnet spectrometer, designed to register the fluxes of charged particles and non-stationary phenomena in cosmic ray research, is installed on the side of the satellite. While folded aginst the telescope for launch it is rotated 180° after reaching orbit pointig upwards along the service module.

Also on board is the Russian 9 kg ARINA research hardware for detection of high-energetic electrons and protons, their identification, detection of high-energetic particles bursts ? earthquake signs. It consists of a spectrometer and a particle detector for the observation of solar-magnetosphere variations of charged particle fluxes.

The satellite was initially placed in a 355 by 573 km orbit in 2006. On 10 September 2010, its orbit was circularised to 567 by 573 km, with an inclination of 69.9 degrees.

Satellite COSPAR Date LS Launch Vehicle Remarks
RESURS DK-1 2006-021A 2006-06-15 TTMTR Soyuz-U