CZ-3B R/B
NORAD 43247
Rocket Body
MEO
2018-029C
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MEO · NORAD 43247
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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
325 km
Apogee
16920 km
Inclination
54.9°
Period
304.7 min
Mean Motion
4.72573861 rev/day
TLE Epoch
2026-06-25 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude8,623 km
Orbital Velocity18,562 km/h
Velocity5.16 km/s
Orbital Period5 hours 5 minutes
Orbits / Day4.73
Eccentricity0.5534
Semi-Major Axis14,994 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2018-03-29
Launch Site
Xichang, China
Int'l Designator
2018-029C
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 2018-03-29 from Xichang, China on the Beidou-3 launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 325 km and 16,920 km with an inclination of 54.9°. It travels at approximately 18,562 km/h (5.16 km/s), completing one full orbit every 5 hours 5 minutes — that’s roughly 4.73 orbits per day. Its orbital eccentricity of 0.5534 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 8,623 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 12 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 54.9°, CZ-3B R/B passes over latitudes between 54.9°N and 54.9°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. 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 325 km (perigee) and 16,920 km (apogee), with an average altitude of approximately 8,623 km. It completes one orbit every 5 hours 5 minutes, travelling at approximately 18,562 km/h (11,534 mph).
CZ-3B R/B (NORAD ID 43247) 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 2018-03-29 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 43247) 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 18,562 km/h (11,534 mph) — roughly 5.16 km/s. It completes 4.73 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 9 sunrises and sunsets every 24 hours.