Official name COROT
Alternative name COROT
Cospar ID 2006-063A
Norad ID 29678
Launch date 2006-12-27
Launch site TTMTR
Launch vehicle Souyz-2-1b Fregat
Country/Organization France, Europe
Type application Astronomy
Operator CNES, ESA
RCS size LARGE
Decay date ON ORBIT
Period (min) 99.51
Inclination (deg) 90.08
Perigee (km) 599
Apogee (km) 872
Eccentricity 0.185588035350102
Mean motion (revs. per day) 14.4709074464878
Semi-Major axis (km) 7113.635
Raan (deg) 29.1441
Arg of perigee (deg) 244.0862
Shape Cyl + 2 Pan
Mass (kg) 605
Diameter (m) 2
Height (m) 9
Span (m^2) 9
Lifetime 2.5 years (minimum), 3 years (planned), 6 years (achieved)
Contractors Alcatel Space
Equipment 27 cm diameter telescope
Configuration Proteus Bus
Power 2 deployable solar arrays, batteries

The COROT (Convection Rotation à Transits planétaires / Convection Rotation and planetary Transits) instrument, an afocal telescope equipped by four CCD detectors, was put on a Proteus platform and launched in late 2006 for an at least 2 and 1/2 years mission.

COROT has two scientific objectives:

  • The detection and the study of stars vibrations (stellar seismology).
  • The search for extrasolar planets and more particularly the telluric planets.

This astrophysical space experiment will enable to study, in two application domains, phenomena and objects never observed to this day.

The payload main components are:

  • The afocal telescope is at first constituted of two parabolic mirrors allowing to decrease 3 times the equivalent entry pupil diameter, then 6 dioptric lens allowing to have a 1.1 m focal length.
    The field of view is a square of 2.8 × 2.8°, half for the seismology mission, the other half for the exoplanet mission.
  • The focal plane detectors are 4 CCDs and working in the visible in the MPP mode. They are installed in the focal box, which temperature is -40° C with a variation lower than 0.05° C/hour.
    For the seismology mission, the image spot for a star will be spread out on about 400 pixels, exposure time of 1 second,
    A prism, allowing to get a color image of the stars, will be installed before the exoplanet field. It will enable to distinguish the stellar activities of a planetary transit, for the brightest stars.
  • The external baffle was designed to have a reduction coefficient of 10-13. Thus, the maximum number of photons coming from the Earth is 0,2 photon/pixel/second, if the Earth is at least 20° from the telescope axis. This baffle is protected during the launch by a one shot shutter.

COROT stopped sending data on 2. November 2012 due to a computer failure. Attempts to revive the observatory failed and the mission was terminated in June 2013. The satellite was finally switched off on 17 June 2014.

Satellite COSPAR Date LS Launch Vehicle Remarks
COROT 2006-063A 2006-12-27 TTMTR Souyz-2-1b Fregat