CZ-6A R/B
NORAD 63922
Rocket Body
LEO
2025-096E
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LEO · NORAD 63922
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🛰️ Orbital Parameters
Perigee
629 km
Apogee
730 km
Inclination
86.0°
Period
98.3 min
Mean Motion
14.64171016 rev/day
TLE Epoch
2026-06-25 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude680 km
Orbital Velocity27,068 km/h
Velocity7.52 km/s
Orbital Period98 minutes
Orbits / Day14.64
Eccentricity0.0072
Semi-Major Axis7,051 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-05-11
Launch Site
Taiyuan, China
Int'l Designator
2025-096E
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 629 km and 730 km with an inclination of 86.0°. It travels at approximately 27,068 km/h (7.52 km/s), completing one full orbit every 98 minutes — that’s roughly 14.64 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 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 680 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-6A R/B’s average altitude, there are currently 329 active payloads and 1,265 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. 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 72 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 629 km (perigee) and 730 km (apogee), with an average altitude of approximately 680 km. It completes one orbit every 98 minutes, travelling at approximately 27,068 km/h (16,819 mph).
CZ-6A R/B (NORAD ID 63922) 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-6A R/B (NORAD ID 63922) 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 27,068 km/h (16,819 mph) — roughly 7.52 km/s. It completes 14.64 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.