CZ-4C R/B
NORAD 36123
Rocket Body
LEO
2009-072C
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LEO · NORAD 36123
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
970 km
Apogee
1203 km
Inclination
100.5°
Period
107.0 min
Mean Motion
13.46238861 rev/day
TLE Epoch
2026-06-26 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,087 km
Orbital Velocity26,319 km/h
Velocity7.31 km/s
Orbital Period107 minutes
Orbits / Day13.46
Eccentricity0.0156
Semi-Major Axis7,458 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2009-12-15
Launch Site
Taiyuan, China
Int'l Designator
2009-072C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-4C R/B is a spent rocket body associated with China, launched on 2009-12-15 from Taiyuan, China on the yaogan weixing bahao launch. After 17 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 970 km and 1,203 km with an inclination of 100.5°. It travels at approximately 26,319 km/h (7.31 km/s), completing one full orbit every 107 minutes — that’s roughly 13.46 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Spent rocket bodies like CZ-4C R/B 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
CZ-4C R/B orbits at an average altitude of 1,087 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of CZ-4C R/B’s average altitude, there are currently 182 active payloads and 401 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 100.5°, CZ-4C R/B passes over latitudes between 100.5°N and 100.5°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. China operates approximately 1,221 active satellites in total, of which 160 share a similar altitude band with CZ-4C R/B.
🔗 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
CZ-4C R/B orbits in Low Earth Orbit (LEO) at altitudes between 970 km (perigee) and 1,203 km (apogee), with an average altitude of approximately 1,087 km. It completes one orbit every 107 minutes, travelling at approximately 26,319 km/h (16,354 mph).
CZ-4C R/B (NORAD ID 36123) 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.
CZ-4C R/B was launched on 2009-12-15 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4C R/B (NORAD ID 36123) 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.
CZ-4C R/B travels at approximately 26,319 km/h (16,354 mph) — roughly 7.31 km/s. It completes 13.46 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.