TJS-19 AKM
NORAD 64094
Rocket Body
GEO
2025-097C
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GEO · NORAD 64094
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Altitude (km)
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Latitude
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🛰️ Orbital Parameters
Perigee
36132 km
Apogee
36256 km
Inclination
3.3°
Period
1457.0 min
Mean Motion
0.98836468 rev/day
TLE Epoch
2026-06-25 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,194 km
Orbital Velocity11,017 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0015
Semi-Major Axis42,565 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-05-12
Launch Site
Xichang, China
Int'l Designator
2025-097C
Object Type
Rocket Body
RCS Size
Unknown
📖 About This Object
TJS-19 AKM is a spent rocket body associated with China, launched on 2025-05-12 from Xichang, China on the TJS 19 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Geostationary Orbit (GEO) at altitudes between 36,132 km and 36,256 km with an inclination of 3.3°. It travels at approximately 11,017 km/h (3.06 km/s), completing one full orbit every 24.3 hours — 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 TJS-19 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-19 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 3.3°, 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 TJS-19 AKM’s average altitude, there are currently 118 active payloads and 14 tracked debris or rocket body fragments. China operates approximately 1,221 active satellites in total, of which 5 share a similar altitude band with TJS-19 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-19 AKM orbits at approximately 36,194 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 11,017 km/h — it just keeps pace with the ground below. With an inclination of 3.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
TJS-19 AKM (NORAD ID 64094) 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-19 AKM was launched on 2025-05-12 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks TJS-19 AKM (NORAD ID 64094) 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-19 AKM travels at approximately 11,017 km/h (6,845 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.