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CZ-4C R/B

NORAD 43278 Rocket Body LEO 2018-034D
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🛰️ Orbital Parameters
Perigee
740 km
Apogee
1325 km
Inclination
63.4°
Period
105.8 min
Mean Motion
13.60963407 rev/day
TLE Epoch
2026-10-15 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,033 km
Orbital Velocity26,415 km/h
Velocity7.34 km/s
Orbital Period106 minutes
Orbits / Day13.61
Eccentricity0.0395
Semi-Major Axis7,404 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2018-04-10
Launch Site
Jiuquan Satellite Launch Center, China
Int'l Designator
2018-034D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-4C R/B is a spent rocket body associated with China, launched on 2018-04-10 from Jiuquan Satellite Launch Center, China on the YG-31-01 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 740 km and 1,325 km with an inclination of 63.4°. It travels at approximately 26,415 km/h (7.34 km/s), completing one full orbit every 106 minutes — that’s roughly 13.61 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Spent rocket bodies like CZ-4C 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-4C R/B orbits at an average altitude of 1,033 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of CZ-4C R/B’s average altitude, there are currently 347 active payloads and 757 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 63.4°, CZ-4C R/B passes over latitudes between 63.4°N and 63.4°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,321 active satellites in total, of which 207 share a similar altitude band with CZ-4C R/B.
🔗 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-4C R/B orbits in Low Earth Orbit (LEO) at altitudes between 740 km (perigee) and 1,325 km (apogee), with an average altitude of approximately 1,033 km. It completes one orbit every 106 minutes, travelling at approximately 26,415 km/h (16,414 mph).
CZ-4C R/B (NORAD ID 43278) 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-4C R/B was launched on 2018-04-10 from Jiuquan Satellite Launch Center, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4C R/B (NORAD ID 43278) 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-4C R/B travels at approximately 26,415 km/h (16,414 mph) — roughly 7.34 km/s. It completes 13.61 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.