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METEOSAT 1 AKM

NORAD 13907 Rocket Body GEO 1977-108D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36095 km
Apogee
36893 km
Inclination
6.3°
Period
1472.4 min
Mean Motion
0.97799268 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,494 km
Orbital Velocity10,978 km/h
Velocity3.05 km/s
Orbital Period24.5 hours
Orbits / Day0.98
Eccentricity0.0093
Semi-Major Axis42,865 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
EUMETSAT (ESA (European Space Agency))
Launch Date
1977-11-23
Launch Site
Cape Canaveral, Florida
Int'l Designator
1977-108D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
weather
📖 About This Object
METEOSAT 1 AKM is a spent rocket body associated with ESA (European Space Agency), launched on 1977-11-23 from Cape Canaveral, Florida. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,095 km and 36,893 km with an inclination of 6.3°. It travels at approximately 10,978 km/h (3.05 km/s), completing one full orbit every 24.5 hours — that’s roughly 0.98 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 1 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 1 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 6.3°, 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 1 AKM’s average altitude, there are currently 11 active payloads and 25 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 1 AKM orbits at approximately 36,494 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 10,978 km/h — it just keeps pace with the ground below. With an inclination of 6.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
METEOSAT 1 AKM (NORAD ID 13907) 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 1 AKM was launched on 1977-11-23 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks METEOSAT 1 AKM (NORAD ID 13907) 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 1 AKM travels at approximately 10,978 km/h (6,821 mph) — roughly 3.05 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.