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CZ-8 R/B

NORAD 63177 Rocket Body LEO 2025-046U
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
814 km
Apogee
907 km
Inclination
89.0°
Period
102.2 min
Mean Motion
14.09654522 rev/day
TLE Epoch
2026-06-25 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude861 km
Orbital Velocity26,727 km/h
Velocity7.42 km/s
Orbital Period102 minutes
Orbits / Day14.10
Eccentricity0.0064
Semi-Major Axis7,232 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-03-11
Launch Site
Wenchang, China
Int'l Designator
2025-046U
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-8 R/B is a spent rocket body associated with China, launched on 2025-03-11 from Wenchang, China on the Qianfan 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 814 km and 907 km with an inclination of 89.0°. It travels at approximately 26,727 km/h (7.42 km/s), completing one full orbit every 102 minutes — that’s roughly 14.10 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Spent rocket bodies like CZ-8 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-8 R/B orbits at an average altitude of 861 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-8 R/B’s average altitude, there are currently 224 active payloads and 1,923 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 89.0°, CZ-8 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 105 share a similar altitude band with CZ-8 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-8 R/B orbits in Low Earth Orbit (LEO) at altitudes between 814 km (perigee) and 907 km (apogee), with an average altitude of approximately 861 km. It completes one orbit every 102 minutes, travelling at approximately 26,727 km/h (16,608 mph).
CZ-8 R/B (NORAD ID 63177) 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-8 R/B was launched on 2025-03-11 from Wenchang, China, China’s newest coastal launch facility on Hainan Island, used for heavy-lift Long March 5 missions. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-8 R/B (NORAD ID 63177) 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-8 R/B travels at approximately 26,727 km/h (16,608 mph) — roughly 7.42 km/s. It completes 14.10 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.