FENGYUN 2B AKM
NORAD 26460
Rocket Body
GEO
2000-032C
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GEO · NORAD 26460
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
35708 km
Apogee
35903 km
Inclination
14.4°
Period
1437.1 min
Mean Motion
1.00203333 rev/day
TLE Epoch
2026-06-24 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,806 km
Orbital Velocity11,067 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0023
Semi-Major Axis42,177 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
2000-06-25
Launch Site
Xichang, China
Int'l Designator
2000-032C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
FENGYUN 2B AKM is a spent rocket body associated with China, launched on 2000-06-25 from Xichang, China on the Feng Yun Er Yi launch. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,708 km and 35,903 km with an inclination of 14.4°. It travels at approximately 11,067 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 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 2B 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 2B 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 14.4°, 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 2B AKM’s average altitude, there are currently 712 active payloads and 64 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. China operates approximately 1,221 active satellites in total, of which 112 share a similar altitude band with FENGYUN 2B 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 2B AKM orbits at approximately 35,806 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 11,067 km/h — it just keeps pace with the ground below. With an inclination of 14.4°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
FENGYUN 2B AKM (NORAD ID 26460) 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 2B AKM was launched on 2000-06-25 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 2B AKM (NORAD ID 26460) 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 2B AKM travels at approximately 11,067 km/h (6,877 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.