CZ-4C R/B
NORAD 47696
Rocket Body
LEO
2021-014F
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LEO · NORAD 47696
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
777 km
Apogee
1233 km
Inclination
63.5°
Period
105.2 min
Mean Motion
13.68602929 rev/day
TLE Epoch
2026-10-15 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,005 km
Orbital Velocity26,464 km/h
Velocity7.35 km/s
Orbital Period105 minutes
Orbits / Day13.69
Eccentricity0.0309
Semi-Major Axis7,376 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2021-02-24
Launch Site
Jiuquan Satellite Launch Center, China
Int'l Designator
2021-014F
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 2021-02-24 from Jiuquan Satellite Launch Center, China on the Yaogan 31-03 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 777 km and 1,233 km with an inclination of 63.5°. It travels at approximately 26,464 km/h (7.35 km/s), completing one full orbit every 105 minutes — that’s roughly 13.69 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 1,005 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 276 active payloads and 1,057 tracked debris or rocket body fragments. With an inclination of 63.5°, CZ-4C R/B passes over latitudes between 63.5°N and 63.5°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,320 active satellites in total, of which 38 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 777 km (perigee) and 1,233 km (apogee), with an average altitude of approximately 1,005 km. It completes one orbit every 105 minutes, travelling at approximately 26,464 km/h (16,444 mph).
CZ-4C R/B (NORAD ID 47696) 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 2021-02-24 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 47696) 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 26,464 km/h (16,444 mph) — roughly 7.35 km/s. It completes 13.69 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.