CZ-5 R/B
NORAD 59021
Rocket Body
MEO
2024-037B
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MEO · NORAD 59021
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
238 km
Apogee
31509 km
Inclination
16.3°
Period
550.6 min
Mean Motion
2.61547813 rev/day
TLE Epoch
2026-10-14 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude15,874 km
Orbital Velocity15,239 km/h
Velocity4.23 km/s
Orbital Period9 hours 11 minutes
Orbits / Day2.62
Eccentricity0.7029
Semi-Major Axis22,245 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2024-02-23
Launch Site
Wenchang Space Launch Site, China
Int'l Designator
2024-037B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-5 R/B is a spent rocket body associated with China, launched on 2024-02-23 from Wenchang Space Launch Site, China on the TJS 11 launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 238 km and 31,509 km with an inclination of 16.3°. It travels at approximately 15,239 km/h (4.23 km/s), completing one full orbit every 9 hours 11 minutes — that’s roughly 2.62 orbits per day. Its orbital eccentricity of 0.7029 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like CZ-5 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-5 R/B orbits at an average altitude of 15,874 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of CZ-5 R/B’s average altitude, there are currently 1 active payload and 9 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 16.3°, CZ-5 R/B passes over latitudes between 16.3°N and 16.3°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. China operates approximately 1,320 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
CZ-5 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 238 km (perigee) and 31,509 km (apogee), with an average altitude of approximately 15,874 km. It completes one orbit every 9 hours 11 minutes, travelling at approximately 15,239 km/h (9,469 mph).
CZ-5 R/B (NORAD ID 59021) 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-5 R/B was launched on 2024-02-23 from Wenchang Space Launch Site, China, China’s newest coastal launch facility on Hainan Island, used for heavy-lift Long March 5 missions. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-5 R/B (NORAD ID 59021) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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-5 R/B travels at approximately 15,239 km/h (9,469 mph) — roughly 4.23 km/s. It completes 2.62 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.