CZ-4C R/B
NORAD 65234
Rocket Body
LEO
2025-177B
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LEO · NORAD 65234
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
593 km
Apogee
806 km
Inclination
11.0°
Period
98.8 min
Mean Motion
14.57949749 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude700 km
Orbital Velocity27,030 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.58
Eccentricity0.0151
Semi-Major Axis7,071 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-08-17
Launch Site
Xichang, China
Int'l Designator
2025-177B
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 2025-08-17 from Xichang, China on the SY28B-02 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 593 km and 806 km with an inclination of 11.0°. It travels at approximately 27,030 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.58 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 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 700 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of CZ-4C R/B’s average altitude, there are currently 273 active payloads and 1,472 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 11.0°, CZ-4C R/B passes over latitudes between 11.0°N and 11.0°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. China operates approximately 1,221 active satellites in total, of which 58 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 593 km (perigee) and 806 km (apogee), with an average altitude of approximately 700 km. It completes one orbit every 99 minutes, travelling at approximately 27,030 km/h (16,796 mph).
CZ-4C R/B (NORAD ID 65234) 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 2025-08-17 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4C R/B (NORAD ID 65234) 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 27,030 km/h (16,796 mph) — roughly 7.51 km/s. It completes 14.58 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.