CZ-3B R/B
NORAD 62486
Rocket Body
MEO
2025-002B
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
141 km
Apogee
14692 km
Inclination
28.4°
Period
268.8 min
Mean Motion
5.35822806 rev/day
TLE Epoch
2026-06-24 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude7,417 km
Orbital Velocity19,357 km/h
Velocity5.38 km/s
Orbital Period4 hours 29 minutes
Orbits / Day5.36
Eccentricity0.5277
Semi-Major Axis13,788 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-01-06
Launch Site
Xichang, China
Int'l Designator
2025-002B
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 2025-01-06 from Xichang, China on the Shi Jian 25 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Medium Earth Orbit (MEO) at altitudes between 141 km and 14,692 km with an inclination of 28.4°. It travels at approximately 19,357 km/h (5.38 km/s), completing one full orbit every 4 hours 29 minutes — that’s roughly 5.36 orbits per day. Its orbital eccentricity of 0.5277 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 7,417 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 14 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 28.4°, CZ-3B R/B passes over latitudes between 28.4°N and 28.4°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 1,221 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 141 km (perigee) and 14,692 km (apogee), with an average altitude of approximately 7,417 km. It completes one orbit every 4 hours 29 minutes, travelling at approximately 19,357 km/h (12,028 mph).
CZ-3B R/B (NORAD ID 62486) 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 2025-01-06 from Xichang, 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 62486) 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-3B R/B travels at approximately 19,357 km/h (12,028 mph) — roughly 5.38 km/s. It completes 5.36 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 11 sunrises and sunsets every 24 hours.