CLUSTER II-FM8
NORAD 26464
Payload
HEO
2000-045B
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HEO · NORAD 26464
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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
464 km
Apogee
131898 km
Inclination
150.2°
Period
3241.9 min
Mean Motion
0.44418308 rev/day
TLE Epoch
2026-06-15 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude66,181 km
Orbital Velocity8,438 km/h
Velocity2.34 km/s
Orbital Period54.0 hours
Orbits / Day0.44
Eccentricity0.9058
Semi-Major Axis72,552 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
European Space Agency (ESA) (and 250 international scientific investigators) (ESA (European Space Agency))
Launch Date
2000-08-09
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2000-045B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
CLUSTER II-FM8 is an active satellite operated by European Space Agency (ESA) (and 250 international scientific investigators) (ESA (European Space Agency)), launched on 2000-08-09 from Baikonur, Kazakhstan. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 464 km and 131,898 km with an inclination of 150.2°. It travels at approximately 8,438 km/h (2.34 km/s), completing one full orbit every 54.0 hours — that’s roughly 0.44 orbits per day. Its orbital eccentricity of 0.9058 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks CLUSTER II-FM8 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CLUSTER II-FM8 follows a Highly Elliptical Orbit, sweeping between 464 km (perigee) and 131,898 km (apogee). It spends most of its 54.0 hours orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. With an inclination of 150.2°, CLUSTER II-FM8 passes over latitudes between 150.2°N and 150.2°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. ESA (European Space Agency) operates approximately 93 active satellites in total.
❓ Frequently Asked Questions
CLUSTER II-FM8 follows a Highly Elliptical Orbit, swinging between 464 km (perigee) and 131,898 km (apogee). It spends most of its 54.0 hours orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
CLUSTER II-FM8 is operated by European Space Agency (ESA) (and 250 international scientific investigators) (ESA (European Space Agency)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26464. You can track CLUSTER II-FM8 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CLUSTER II-FM8 was launched on 2000-08-09 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: permanent — geostationary orbit, no atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks CLUSTER II-FM8 (NORAD ID 26464) 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.
CLUSTER II-FM8’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 8,438 km/h (2.34 km/s), completing one revolution every 54.0 hours. Learn more about highly elliptical orbits.