METEOSAT 4 AKM
NORAD 20800
Rocket Body
GEO
1989-020E
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GEO · NORAD 20800
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
35191 km
Apogee
36279 km
Inclination
11.0°
Period
1433.5 min
Mean Motion
1.00456123 rev/day
TLE Epoch
2026-06-18 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,735 km
Orbital Velocity11,076 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0129
Semi-Major Axis42,106 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
EUMETSAT (ESA (European Space Agency))
Launch Date
1989-03-06
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1989-020E
Object Type
Rocket Body
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
weather
📖 About This Object
METEOSAT 4 AKM is a spent rocket body associated with ESA (European Space Agency), launched on 1989-03-06 from Guiana Space Centre, Kourou. With over 37 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,191 km and 36,279 km with an inclination of 11.0°. It travels at approximately 11,076 km/h (3.08 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. It is part of the Weather constellation group. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Spent rocket bodies like METEOSAT 4 AKM are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
METEOSAT 4 AKM occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 11.0°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of METEOSAT 4 AKM’s average altitude, there are currently 85 active payloads and 42 tracked debris or rocket body fragments. ESA (European Space Agency) operates approximately 93 active satellites in total.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
METEOSAT 4 AKM orbits at approximately 35,735 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,076 km/h — it just keeps pace with the ground below. With an inclination of 11.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
METEOSAT 4 AKM (NORAD ID 20800) is a spent rocket body — the upper stage of a launch vehicle attributed to ESA (European Space Agency). It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
METEOSAT 4 AKM was launched on 1989-03-06 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. View the full satellite launch log.
Yes — Orbital Radar tracks METEOSAT 4 AKM (NORAD ID 20800) 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.
METEOSAT 4 AKM travels at approximately 11,076 km/h (6,883 mph) — roughly 3.08 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.