CZ-3B R/B
NORAD 59916
Rocket Body
MEO
2024-104B
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MEO · NORAD 59916
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
173 km
Apogee
23551 km
Inclination
26.7°
Period
408.6 min
Mean Motion
3.52635251 rev/day
TLE Epoch
2026-10-17 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude11,862 km
Orbital Velocity16,832 km/h
Velocity4.68 km/s
Orbital Period6 hours 49 minutes
Orbits / Day3.53
Eccentricity0.6411
Semi-Major Axis18,233 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2024-05-30
Launch Site
Xichang Satellite Launch Center, China
Int'l Designator
2024-104B
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 2024-05-30 from Xichang Satellite Launch Center, China on the Paksat-MM1 launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 173 km and 23,551 km with an inclination of 26.7°. It travels at approximately 16,832 km/h (4.68 km/s), completing one full orbit every 6 hours 49 minutes — that’s roughly 3.53 orbits per day. Its orbital eccentricity of 0.6411 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 11,862 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 2 active payloads and 5 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 26.7°, CZ-3B R/B passes over latitudes between 26.7°N and 26.7°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. China operates approximately 1,325 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 173 km (perigee) and 23,551 km (apogee), with an average altitude of approximately 11,862 km. It completes one orbit every 6 hours 49 minutes, travelling at approximately 16,832 km/h (10,459 mph).
CZ-3B R/B (NORAD ID 59916) 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 2024-05-30 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 59916) 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 16,832 km/h (10,459 mph) — roughly 4.68 km/s. It completes 3.53 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 7 sunrises and sunsets every 24 hours.