CZ-3C R/B
NORAD 43875
Rocket Body
MEO
2018-110B
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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
219 km
Apogee
25466 km
Inclination
28.0°
Period
442.0 min
Mean Motion
3.25871031 rev/day
TLE Epoch
2026-07-16 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude12,843 km
Orbital Velocity16,397 km/h
Velocity4.55 km/s
Orbital Period7 hours 22 minutes
Orbits / Day3.26
Eccentricity0.6570
Semi-Major Axis19,214 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2018-12-24
Launch Site
Xichang, China
Int'l Designator
2018-110B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-3C R/B is a spent rocket body associated with China, launched on 2018-12-24 from Xichang, China on the TJS 3 launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 219 km and 25,466 km with an inclination of 28.0°. It travels at approximately 16,397 km/h (4.55 km/s), completing one full orbit every 7 hours 22 minutes — that’s roughly 3.26 orbits per day. Its orbital eccentricity of 0.6570 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like CZ-3C 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-3C R/B orbits at an average altitude of 12,843 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-3C R/B’s average altitude, there are currently 0 active payloads and 4 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 28.0°, CZ-3C R/B passes over latitudes between 28.0°N and 28.0°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 1,247 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-3C R/B orbits in Medium Earth Orbit (MEO) at altitudes between 219 km (perigee) and 25,466 km (apogee), with an average altitude of approximately 12,843 km. It completes one orbit every 7 hours 22 minutes, travelling at approximately 16,397 km/h (10,189 mph).
CZ-3C R/B (NORAD ID 43875) 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-3C R/B was launched on 2018-12-24 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-3C R/B (NORAD ID 43875) 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-3C R/B travels at approximately 16,397 km/h (10,189 mph) — roughly 4.55 km/s. It completes 3.26 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 7 sunrises and sunsets every 24 hours.