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FENGYUN 2A AKM

NORAD 25611 Rocket Body GEO 1997-029C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
34138 km
Apogee
36004 km
Inclination
13.8°
Period
1399.7 min
Mean Motion
1.02879287 rev/day
TLE Epoch
2026-06-26 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,071 km
Orbital Velocity11,165 km/h
Velocity3.10 km/s
Orbital Period23 hours 20 minutes
Orbits / Day1.03
Eccentricity0.0225
Semi-Major Axis41,442 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
1997-06-10
Launch Site
Xichang, China
Int'l Designator
1997-029C
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
FENGYUN 2A AKM is a spent rocket body associated with China, launched on 1997-06-10 from Xichang, China on the Feng Yun Er Jia launch. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 34,138 km and 36,004 km with an inclination of 13.8°. It travels at approximately 11,165 km/h (3.10 km/s), completing one full orbit every 23 hours 20 minutes — that’s roughly 1.03 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 2A 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 2A 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 13.8°, 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 2A AKM’s average altitude, there are currently 0 active payloads and 11 tracked debris or rocket body fragments. China operates approximately 1,221 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
FENGYUN 2A AKM orbits at approximately 35,071 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 11,165 km/h — it just keeps pace with the ground below. With an inclination of 13.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
FENGYUN 2A AKM (NORAD ID 25611) 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 2A AKM was launched on 1997-06-10 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 2A AKM (NORAD ID 25611) 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 2A AKM travels at approximately 11,165 km/h (6,937 mph) — roughly 3.10 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.