CZ-12 R/B
NORAD 67068
Rocket Body
LEO
2025-295K
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LEO · NORAD 67068
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Longitude
🛰️ Orbital Parameters
Perigee
714 km
Apogee
795 km
Inclination
50.0°
Period
99.9 min
Mean Motion
14.41219170 rev/day
TLE Epoch
2026-06-25 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude755 km
Orbital Velocity26,925 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.41
Eccentricity0.0057
Semi-Major Axis7,126 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-12-11
Launch Site
Wenchang, China
Int'l Designator
2025-295K
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 2025-12-11 from Wenchang, China on the WHDW 16 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 714 km and 795 km with an inclination of 50.0°. It travels at approximately 26,925 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.41 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 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 755 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-12 R/B’s average altitude, there are currently 355 active payloads and 2,004 tracked debris or rocket body fragments. 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 51 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 714 km (perigee) and 795 km (apogee), with an average altitude of approximately 755 km. It completes one orbit every 100 minutes, travelling at approximately 26,925 km/h (16,731 mph).
CZ-12 R/B (NORAD ID 67068) 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 2025-12-11 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-12 R/B (NORAD ID 67068) 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 26,925 km/h (16,731 mph) — roughly 7.48 km/s. It completes 14.41 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.