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CZ-3B R/B

NORAD 41587 Rocket Body MEO 2016-037B
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🛰️ Orbital Parameters
Perigee
188 km
Apogee
17107 km
Inclination
19.4°
Period
305.5 min
Mean Motion
4.71187998 rev/day
TLE Epoch
2026-10-13 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude8,648 km
Orbital Velocity18,546 km/h
Velocity5.15 km/s
Orbital Period5 hours 6 minutes
Orbits / Day4.71
Eccentricity0.5633
Semi-Major Axis15,019 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2016-06-12
Launch Site
Xichang Satellite Launch Center, China
Int'l Designator
2016-037B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-3B R/B is a spent rocket body associated with China, launched on 2016-06-12 from Xichang Satellite Launch Center, China on the Beidou G7 launch. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 188 km and 17,107 km with an inclination of 19.4°. It travels at approximately 18,546 km/h (5.15 km/s), completing one full orbit every 5 hours 6 minutes — that’s roughly 4.71 orbits per day. Its orbital eccentricity of 0.5633 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like CZ-3B 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-3B R/B orbits at an average altitude of 8,648 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-3B R/B’s average altitude, there are currently 0 active payloads and 15 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 19.4°, CZ-3B R/B passes over latitudes between 19.4°N and 19.4°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. China operates approximately 1,321 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-3B R/B orbits in Medium Earth Orbit (MEO) at altitudes between 188 km (perigee) and 17,107 km (apogee), with an average altitude of approximately 8,648 km. It completes one orbit every 5 hours 6 minutes, travelling at approximately 18,546 km/h (11,524 mph).
CZ-3B R/B (NORAD ID 41587) 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-3B R/B was launched on 2016-06-12 from Xichang Satellite Launch Center, China. 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-3B R/B (NORAD ID 41587) 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-3B R/B travels at approximately 18,546 km/h (11,524 mph) — roughly 5.15 km/s. It completes 4.71 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 9 sunrises and sunsets every 24 hours.