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TJS-3 AKM

NORAD 43917 Rocket Body GEO 2018-110C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36309 km
Apogee
36357 km
Inclination
4.7°
Period
1464.1 min
Mean Motion
0.98354047 rev/day
TLE Epoch
2026-06-26 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,333 km
Orbital Velocity10,999 km/h
Velocity3.06 km/s
Orbital Period24.4 hours
Orbits / Day0.98
Eccentricity0.0006
Semi-Major Axis42,704 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Academy of Space Technology (CAST) (China)
Launch Date
2018-12-24
Launch Site
Xichang, China
Int'l Designator
2018-110C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
TJS-3 AKM is a spent rocket body associated with China, launched on 2018-12-24 from Xichang, China on the TJS 3 launch. It orbits in Geostationary Orbit (GEO) at altitudes between 36,309 km and 36,357 km with an inclination of 4.7°. It travels at approximately 10,999 km/h (3.06 km/s), completing one full orbit every 24.4 hours — that’s roughly 0.98 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 TJS-3 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
TJS-3 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 4.7°, 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 TJS-3 AKM’s average altitude, there are currently 42 active payloads and 8 tracked debris or rocket body fragments. China operates approximately 1,221 active satellites in total, of which 2 share a similar altitude band with TJS-3 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
TJS-3 AKM orbits at approximately 36,333 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 10,999 km/h — it just keeps pace with the ground below. With an inclination of 4.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
TJS-3 AKM (NORAD ID 43917) 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.
TJS-3 AKM was launched on 2018-12-24 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks TJS-3 AKM (NORAD ID 43917) 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.
TJS-3 AKM travels at approximately 10,999 km/h (6,834 mph) — roughly 3.06 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.