Official name KOMPASS
Alternative name Kompas
Cospar ID 2001-056B
Norad ID 27002
Launch date 2001-12-10
Launch site TTMTR
Launch vehicle Zenit-2
Country/Organization Russia
Type application Earth Sciences
Operator Izmiran
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 105.07
Inclination (deg) 99.71
Perigee (km) 984
Apogee (km) 1012
Eccentricity 0.0140280561122244
Mean motion (revs. per day) 13.7051489483202
Semi-Major axis (km) 7376.135
Raan (deg) 283.6649
Arg of perigee (deg) 306.8573
Shape Trunc Poly + 4 Pan
Mass (kg) 80
Height (m) 0.8
Width (m) 0.6
Depth (m) 0.5
Span (m^2) 0.8
Contractors GRTsKB Makeyev
Power 2 deployabe fixed solar arrays, solar cells, batteries

Compass (Complex Orbital Magneto-Plasma Autonomous Small Satellite) or Kompas (Kompleksniy Orbital'niy Magnito-Plazmenniy Avtonomniy Sputnik) is intended for the detection of the effects of the action of the tectonic breakings of the Earth on the environment, the search for lithospheric, atmospheric and ionospheric responses to changes in the state of the zone of the tectonic activity, which can be important for the prediction/forecast of natural catastrophes, the study of the possibility of the development/detection of the concealed/latent layers of useful minerals - including of oil, gas.

The Kompas 1 satellite was originaly designed to be launched by a Shtil-1 launch vehicle, but was rescheduled for a Zenit-2 piggy-back launch.

Kompas 2 was launched on a Shtil-1. The satellite initially failed to respond to ground commands after launch, but was later put into service when the problem was resolved.

Kompas 2N was to share a launch with Sumbandila (ZA-002) on a Shtil-2.1 vehicle. This launch agreement was cancelled and the satellite remained grounded.

Satellite COSPAR Date LS Launch Vehicle Remarks
KOMPASS 2001-056B 2001-12-10 TTMTR Zenit-2 with Meteor-3M 1, Badr B, Maroc-Tubsat, Reflector
KOMPASS-2 2006-019A 2006-05-26 SADOL Shtil-1