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CZ-6A R/B

NORAD 66051 Rocket Body LEO 2025-233U
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
644 km
Apogee
761 km
Inclination
89.0°
Period
98.8 min
Mean Motion
14.57200854 rev/day
TLE Epoch
2026-06-26 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude703 km
Orbital Velocity27,024 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.57
Eccentricity0.0083
Semi-Major Axis7,074 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-10-17
Launch Site
Taiyuan, China
Int'l Designator
2025-233U
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 2025-10-17 from Taiyuan, China on the Qianfan Jigui 18 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 644 km and 761 km with an inclination of 89.0°. It travels at approximately 27,024 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.57 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 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 703 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 272 active payloads and 1,485 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 89.0°, CZ-6A R/B passes over latitudes between 89.0°N and 89.0°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 60 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 644 km (perigee) and 761 km (apogee), with an average altitude of approximately 703 km. It completes one orbit every 99 minutes, travelling at approximately 27,024 km/h (16,792 mph).
CZ-6A R/B (NORAD ID 66051) 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 2025-10-17 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-6A R/B (NORAD ID 66051) 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 27,024 km/h (16,792 mph) — roughly 7.51 km/s. It completes 14.57 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.