Official name STERKH 2
Alternative name Sterkh No. 12L
Cospar ID 2009-049B
Norad ID 35866
Launch date 2009-09-17
Launch site TTMTR
Launch vehicle Soyuz-2-1b Fregat
Country/Organization Russia
Type application Communications (COSPAS-SARSAT)
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 101.16
Inclination (deg) 98.61
Perigee (km) 811
Apogee (km) 816
Eccentricity 0.00307314074984634
Mean motion (revs. per day) 14.2348754448399
Semi-Major axis (km) 7191.635
Raan (deg) 93.345
Arg of perigee (deg) 10.5519
Shape Box + 2 Pan + 1 Ant
Mass (kg) 171
Height (m) 1.4
Width (m) 0.6
Depth (m) 0.6
Span (m^2) 1.5
Lifetime 5 years
Contractors PO Polyot
Configuration Sterkh Bus
Power 2 deployable fixed solar arrays, batteries

The Sterkh satellites are to replace the Nadezhda series in the international Search and Rescue Satellite-Aided System (COSPAS-SARSAT). Unlike the Nadezhda precursors, the Sterkh series does not provide navigation services, which has been taken over by the GLONASS system. Therefore the satellites can be much smaller and were launched piggy-back on other LEO missions.

The first two satellites were launched in 2009, but both failed shortly after launch. Sterkh 1 failed to properly align its solar panels with the Sun due to a malfunction of the satellite's flight control system resulting in a loss of power. Sterkh 2 failed to properly deploy its stabilisation boom and is therefore not useable for its intended purpose.

Two more satellites were planned for launches in 2013, but were apparently cancelled.

Satellite COSPAR Date LS Launch Vehicle Remarks
STERKH 2009-039B 2009-07-21 PKMTR Kosmos-3M with Kosmos 2454 (Parus #98)
STERKH 2 2009-049B 2009-09-17 TTMTR Soyuz-2-1b Fregat with Meteor-M 1, Universitetsky 2, UGATUSAT, Sumbandila, BLITS, IRIS