CLEMENTINE
NORAD 25978
Payload
LEO
1999-064B
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LEO · NORAD 25978
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
433 km
Apogee
436 km
Inclination
98.2°
Period
93.3 min
Mean Motion
15.44011624 rev/day
TLE Epoch
2026-09-17 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude435 km
Orbital Velocity27,551 km/h
Velocity7.65 km/s
Orbital Period93 minutes
Orbits / Day15.44
Eccentricity0.0002
Semi-Major Axis6,806 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇫🇷 CNES / DGA (France)
Launch Date
1999-12-03
Launch Site
Guiana Space Centre, French Guiana
Int'l Designator
1999-064B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CLEMENTINE is an active satellite operated by CNES / DGA (France), launched on 1999-12-03 from Guiana Space Centre, French Guiana on the Helios 1B launch. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 433 km and 436 km with an inclination of 98.2°. It travels at approximately 27,551 km/h (7.65 km/s), completing one full orbit every 93 minutes — that’s roughly 15.44 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 ~1–3 years. Orbital Radar tracks CLEMENTINE in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CLEMENTINE orbits at an average altitude of 435 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 CLEMENTINE’s average altitude, there are currently 9,765 active payloads and 122 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1017, STARLINK-1039. This makes it one of the more crowded altitude bands, containing roughly 52.2% of all active satellites. With an inclination of 98.2°, CLEMENTINE passes over latitudes between 98.2°N and 98.2°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 124 active satellites in total, of which 11 share a similar altitude band with CLEMENTINE.
❓ Frequently Asked Questions
CLEMENTINE is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 435 km altitude. Its 98.2° 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 93 minutes, travelling at 27,551 km/h.
CLEMENTINE is operated by CNES / DGA (France). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25978. You can track CLEMENTINE in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CLEMENTINE was launched on 1999-12-03 from Guiana Space Centre, French Guiana. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks CLEMENTINE (NORAD ID 25978) 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.
CLEMENTINE travels at approximately 27,551 km/h (17,120 mph) — roughly 7.65 km/s. It completes 15.44 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.