DEMETER
NORAD 28368
Payload
LEO
2004-025C
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LEO · NORAD 28368
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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
616 km
Apogee
619 km
Inclination
98.1°
Period
97.0 min
Mean Motion
14.83758207 rev/day
TLE Epoch
2026-06-18 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude618 km
Orbital Velocity27,188 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.84
Eccentricity0.0002
Semi-Major Axis6,989 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
2004-06-29
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2004-025C
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
DEMETER is an active satellite operated by France, launched on 2004-06-29 from Baikonur, Kazakhstan. With over 22 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 616 km and 619 km with an inclination of 98.1°. It travels at approximately 27,188 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.84 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 DEMETER in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
DEMETER orbits at an average altitude of 618 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 DEMETER’s average altitude, there are currently 1,547 active payloads and 748 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3090, STARLINK-3077. This makes it one of the more crowded altitude bands, containing roughly 8.9% of all active satellites. With an inclination of 98.1°, DEMETER passes over latitudes between 98.1°N and 98.1°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 114 active satellites in total, of which 51 share a similar altitude band with DEMETER.
❓ Frequently Asked Questions
DEMETER is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 618 km altitude. Its 98.1° 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 97 minutes, travelling at 27,188 km/h.
DEMETER is operated by France. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28368. You can track DEMETER in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DEMETER was launched on 2004-06-29 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks DEMETER (NORAD ID 28368) 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.
DEMETER travels at approximately 27,188 km/h (16,894 mph) — roughly 7.55 km/s. It completes 14.84 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.