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Kolibri
Kolibri 2000 Credit: Manufacturer Image |
Russian technology satellite. Kolibri was a joint Russian-Australian educational project to allow school children to monitor low frequency waves and particle fluxes in low orbit.
Status: Operational 2002. First Launch: 2002-03-19. Last Launch: 2002-03-19. Number: 1 . Gross mass: 21 kg (46 lb).
The IKI space science group led the project together with Energia, NPO-M and Polyot. The satellite was equipped with a 2-meter gravity gradient boom and four solar panels. The satellite was ejected into orbit from the Progress M1-7 spacecraft after it had undocked from the International Space Station. in a 385 x 388 km x 51.6 deg orbit.
Subtopics
Family:
Technology,
Technology satellite.
Country:
Russia.
Launch Vehicles:
R-7,
Soyuz-FG.
Launch Sites:
Baikonur,
Baikonur LC1.
Agency:
IKI.
Bibliography:
2,
4,
552,
554.
2002 March 19 - .
22:28 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-FG.
- Kolibri - .
Mass: 21 kg (46 lb). Nation: Russia.
Agency: RAKA.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: Kolibri.
Decay Date: 2002-05-04 . USAF Sat Cat: 27394 . COSPAR: 2001-051C. Apogee: 388 km (241 mi). Perigee: 385 km (239 mi). Inclination: 51.60 deg.
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