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CALIPSO

NORAD 29108 Payload LEO 2006-016B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
662 km
Apogee
664 km
Inclination
98.5°
Period
98.0 min
Mean Motion
14.69354055 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude663 km
Orbital Velocity27,100 km/h
Velocity7.53 km/s
Orbital Period98 minutes
Orbits / Day14.69
Eccentricity0.0001
Semi-Major Axis7,034 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇫🇷 Centre National d'Etudes Spatiales (CNES)/NASA (France)
Launch Date
2006-04-28
Launch Site
Vandenberg SFB, California
Int'l Designator
2006-016B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
CALIPSO is an active satellite operated by Centre National d'Etudes Spatiales (CNES)/NASA (France), launched on 2006-04-28 from Vandenberg SFB, California. With over 20 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 662 km and 664 km with an inclination of 98.5°. It travels at approximately 27,100 km/h (7.53 km/s), completing one full orbit every 98 minutes — that’s roughly 14.69 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks CALIPSO in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CALIPSO orbits at an average altitude of 663 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of CALIPSO’s average altitude, there are currently 649 active payloads and 1,121 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.5°, CALIPSO passes over latitudes between 98.5°N and 98.5°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. France operates approximately 115 active satellites in total, of which 43 share a similar altitude band with CALIPSO.
❓ Frequently Asked Questions
CALIPSO is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 663 km altitude. Its 98.5° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 98 minutes, travelling at 27,100 km/h.
CALIPSO is operated by Centre National d'Etudes Spatiales (CNES)/NASA (France). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 29108. You can track CALIPSO in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CALIPSO was launched on 2006-04-28 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks CALIPSO (NORAD ID 29108) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
CALIPSO travels at approximately 27,100 km/h (16,839 mph) — roughly 7.53 km/s. It completes 14.69 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.