Official name KOLIBRI
Alternative name Kolibri
Cospar ID 2001-051C
Norad ID 27394
Launch date 2001-11-26
Launch site TTMTR
Launch vehicle Soyuz-FG
Country/Organization Russia, Australia
Type application Magnetospheric research, Amateur communication
RCS size MEDIUM
Decay date 2002-05-04
Shape Hex Cyl + 1 Arm
Mass (kg) 27
Diameter (m) 0.2
Height (m) 0.5
Span (m^2) 2
Contractors Space Research Institute (IKI)
Equipment particle analyzer, electrical field analyzer, electrical field flux-gate magnetometer
Propulsion None
Configuration Hexagonal prism, 4 solar arrays, 2 m gravity gradient boom
Power 4 deployable solar arrays, batteries

The Kolibri-2000 microsatellite is an educational microsatellite mission. It was launched from the Progress-M1 7 cargo freighter supply craft to the International Space Station, on it way back to Earth, into a 385 km × 388 km orbit inclined at 51.6 degrees. The spacecraft was designed and manufactured by the Special Design Office of space instrument engineering, Space Research Institute of the Russian Academy of sciences, in collaboration with local space industry. The spacecraft mission is educational, and radio amateur frequencies are employed to return data to participating educational institutions in Obninsk (Russia) and Sydney (Australia). Instruments on board include a flux-gate magnetometer, and a particle and electric field analyser. The spacecraft measures 1.25 m high with a diameter of 0.5 m, carries a 2 m gravity gradient boom and four deployable solar panels.

Satellite COSPAR Date LS Launch Vehicle Remarks
KOLIBRI 2001-051C 2001-11-26 TTMTR Soyuz-FG with Progress-M1 7