CZ-12 R/B
NORAD 67531
Rocket Body
LEO
2026-013K
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
795 km
Apogee
894 km
Inclination
50.0°
Period
101.8 min
Mean Motion
14.14475593 rev/day
TLE Epoch
2026-06-25 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude845 km
Orbital Velocity26,757 km/h
Velocity7.43 km/s
Orbital Period102 minutes
Orbits / Day14.14
Eccentricity0.0069
Semi-Major Axis7,216 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-01-19
Launch Site
Wenchang, China
Int'l Designator
2026-013K
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-12 R/B is a spent rocket body associated with China, launched on 2026-01-19 from Wenchang, China on the WHDW 19 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 795 km and 894 km with an inclination of 50.0°. It travels at approximately 26,757 km/h (7.43 km/s), completing one full orbit every 102 minutes — that’s roughly 14.14 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Spent rocket bodies like CZ-12 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-12 R/B orbits at an average altitude of 845 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-12 R/B’s average altitude, there are currently 233 active payloads and 2,124 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 50.0°, CZ-12 R/B passes over latitudes between 50.0°N and 50.0°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. China operates approximately 1,221 active satellites in total, of which 102 share a similar altitude band with CZ-12 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-12 R/B orbits in Low Earth Orbit (LEO) at altitudes between 795 km (perigee) and 894 km (apogee), with an average altitude of approximately 845 km. It completes one orbit every 102 minutes, travelling at approximately 26,757 km/h (16,626 mph).
CZ-12 R/B (NORAD ID 67531) 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-12 R/B was launched on 2026-01-19 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-12 R/B (NORAD ID 67531) 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-12 R/B travels at approximately 26,757 km/h (16,626 mph) — roughly 7.43 km/s. It completes 14.14 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.