NORAD 29678
COROT
Time
- Local time
- -
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Position
- Latitude
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- Longitude
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- Altitude
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Speed
- Miles per hour
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- Kilometers per second
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- Miles per second
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From your location
- Azimuth
- -
- Elevation
- -
- Right ascension
- -
- Declination
- -
- Local sidereal time
- -
Sunlight
- Day / night
- -
Identity
- NORAD ID
- 29678
- International designator
- 2006-063A
- Launch date
- Dec 27, 2006
- Launch site
- TYURATAM MISSILE AND SPACE COMPLEX
- Radar size (RCS)
- Large (over 1 m²)
Radio
- Uplink
- -
- Downlink
- -
- Beacon
- -
- Mode
- -
Active transmitters from SatNOGS DB, licensed CC BY-SA 4.0.
Your station
- Grid locator
- -
Live
- Azimuth
- -
- Elevation
- -
- Range
- -
- Range rate
- -
- Naked-eye visibility
- -
- Sub-satellite grid
- -
- Footprint diameter
- -
Upcoming passes
Next 48 h · your local timeUse your location to predict passes.
Mutual visibility
With another station · next 48 hUse your location to find mutual windows.
Transmitters
Nominal · add location for Doppler-
Recent receptions
SatNOGS Network-
Orbit data
- TLE epoch
- 2026-11-04 18:01:59 UTC
- TLE age
- -
Radio data from SatNOGS DB and SatNOGS Network, licensed CC BY-SA 4.0.
Its orbit in 3D
Goes round Earth once every 99 minutes, on an orbit tilted 90.1° from the equator, between 602 and 866 km up. Earth is drawn to scale.
Drag to turn · pinch to zoom · it moves live
About COROT
COROT is a satellite from France, launched on Dec 27, 2006 from Tyuratam Missile and Space Complex.
It circles Earth every 99 minutes (14.5 times a day), between 592 and 855 km up, on an orbit tilted 90.1° to the equator, so its path covers latitudes up to 90° north and south.
The map shows where it is right now; the pass list tells you when it next comes over your location.
decommissioned European Space Agency space observatory
- Operated by
- European Space Agency, CNES
- Built by
- Alcatel Space
- Mass
- 668 kg
Wikipedia article ↗ · Names and facts: Wikidata (CC0).
Orbit height over the past year
Over the last 24 days its lowest point went from 591 km to 592 km. Sudden rises are engine burns that lift the orbit; slow declines are drag from the thin upper atmosphere.
From Space-Track element sets, one point a day.