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CZ-6A R/B

NORAD 63921 Rocket Body LEO 2025-096D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
793 km
Apogee
813 km
Inclination
86.0°
Period
100.9 min
Mean Motion
14.26604999 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude803 km
Orbital Velocity26,834 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.27
Eccentricity0.0014
Semi-Major Axis7,174 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-05-11
Launch Site
Taiyuan, China
Int'l Designator
2025-096D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-6A R/B is a spent rocket body associated with China, launched on 2025-05-11 from Taiyuan, China on the Yaogan 40-02 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 793 km and 813 km with an inclination of 86.0°. It travels at approximately 26,834 km/h (7.45 km/s), completing one full orbit every 101 minutes — that’s roughly 14.27 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Spent rocket bodies like CZ-6A 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-6A R/B orbits at an average altitude of 803 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-6A R/B’s average altitude, there are currently 442 active payloads and 2,311 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 86.0°, CZ-6A R/B passes over latitudes between 86.0°N and 86.0°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. China operates approximately 1,221 active satellites in total, of which 105 share a similar altitude band with CZ-6A 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-6A R/B orbits in Low Earth Orbit (LEO) at altitudes between 793 km (perigee) and 813 km (apogee), with an average altitude of approximately 803 km. It completes one orbit every 101 minutes, travelling at approximately 26,834 km/h (16,674 mph).
CZ-6A R/B (NORAD ID 63921) 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-6A R/B was launched on 2025-05-11 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-6A R/B (NORAD ID 63921) 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-6A R/B travels at approximately 26,834 km/h (16,674 mph) — roughly 7.45 km/s. It completes 14.27 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.