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FENGYUN 2D AKM

NORAD 29642 Rocket Body GEO 2006-053C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35586 km
Apogee
36504 km
Inclination
11.8°
Period
1449.3 min
Mean Motion
0.99357061 rev/day
TLE Epoch
2026-06-26 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,045 km
Orbital Velocity11,036 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day0.99
Eccentricity0.0108
Semi-Major Axis42,416 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
2006-12-08
Launch Site
Xichang, China
Int'l Designator
2006-053C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
FENGYUN 2D AKM is a spent rocket body associated with China, launched on 2006-12-08 from Xichang, China on the fengyun erhao D xing launch. With over 20 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,586 km and 36,504 km with an inclination of 11.8°. It travels at approximately 11,036 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 0.99 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Spent rocket bodies like FENGYUN 2D 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
FENGYUN 2D 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 11.8°, 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 FENGYUN 2D AKM’s average altitude, there are currently 92 active payloads and 26 tracked debris or rocket body fragments. China operates approximately 1,221 active satellites in total, of which 6 share a similar altitude band with FENGYUN 2D AKM.
🔗 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
FENGYUN 2D AKM orbits at approximately 36,045 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 11,036 km/h — it just keeps pace with the ground below. With an inclination of 11.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
FENGYUN 2D AKM (NORAD ID 29642) is a spent rocket body — the upper stage of a launch vehicle attributed to China. 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.
FENGYUN 2D AKM was launched on 2006-12-08 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 2D AKM (NORAD ID 29642) 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.
FENGYUN 2D AKM travels at approximately 11,036 km/h (6,857 mph) — roughly 3.07 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.