CERISE
NORAD 23606
Payload
LEO
1995-033B
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LEO · NORAD 23606
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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
457 km
Apogee
464 km
Inclination
98.3°
Period
93.8 min
Mean Motion
15.35240235 rev/day
TLE Epoch
2026-06-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude461 km
Orbital Velocity27,499 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.35
Eccentricity0.0005
Semi-Major Axis6,832 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1995-07-07
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1995-033B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CERISE is an active satellite operated by France, launched on 1995-07-07 from Guiana Space Centre, Kourou. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 457 km and 464 km with an inclination of 98.3°. It travels at approximately 27,499 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.35 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 CERISE in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CERISE orbits at an average altitude of 461 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 CERISE’s average altitude, there are currently 7,969 active payloads and 173 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 45.7% of all active satellites. With an inclination of 98.3°, CERISE passes over latitudes between 98.3°N and 98.3°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 21 share a similar altitude band with CERISE.
❓ Frequently Asked Questions
CERISE is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 461 km altitude. Its 98.3° 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 94 minutes, travelling at 27,499 km/h.
CERISE is operated by France. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23606. You can track CERISE in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CERISE was launched on 1995-07-07 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks CERISE (NORAD ID 23606) 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.
CERISE travels at approximately 27,499 km/h (17,087 mph) — roughly 7.64 km/s. It completes 15.35 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.