CZ-4C R/B
NORAD 40341
Rocket Body
LEO
2014-080D
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LEO · NORAD 40341
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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
602 km
Apogee
1398 km
Inclination
63.4°
Period
105.1 min
Mean Motion
13.69871732 rev/day
TLE Epoch
2026-06-26 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,000 km
Orbital Velocity26,473 km/h
Velocity7.35 km/s
Orbital Period105 minutes
Orbits / Day13.70
Eccentricity0.0540
Semi-Major Axis7,371 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2014-12-10
Launch Site
Jiuquan, China
Int'l Designator
2014-080D
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 2014-12-10 from Jiuquan, China on the YG-25 launch. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 602 km and 1,398 km with an inclination of 63.4°. It travels at approximately 26,473 km/h (7.35 km/s), completing one full orbit every 105 minutes — that’s roughly 13.70 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 1,000 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 236 active payloads and 864 tracked debris or rocket body fragments. 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 1,221 active satellites in total, of which 40 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 602 km (perigee) and 1,398 km (apogee), with an average altitude of approximately 1,000 km. It completes one orbit every 105 minutes, travelling at approximately 26,473 km/h (16,450 mph).
CZ-4C R/B (NORAD ID 40341) 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 2014-12-10 from Jiuquan, 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 40341) 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-4C R/B travels at approximately 26,473 km/h (16,450 mph) — roughly 7.35 km/s. It completes 13.70 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.