CZ-2D R/B
NORAD 54215
Rocket Body
LEO
2022-142B
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LEO · NORAD 54215
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
763 km
Apogee
792 km
Inclination
59.9°
Period
100.4 min
Mean Motion
14.34371962 rev/day
TLE Epoch
2026-06-26 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude778 km
Orbital Velocity26,882 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.34
Eccentricity0.0020
Semi-Major Axis7,149 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2022-10-29
Launch Site
Jiuquan, China
Int'l Designator
2022-142B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-2D R/B is a spent rocket body associated with China, launched on 2022-10-29 from Jiuquan, China on the Shiyan 20C launch. It orbits in Low Earth Orbit (LEO) at altitudes between 763 km and 792 km with an inclination of 59.9°. It travels at approximately 26,882 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.34 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Spent rocket bodies like CZ-2D 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-2D R/B orbits at an average altitude of 778 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-2D R/B’s average altitude, there are currently 419 active payloads and 2,176 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 59.9°, CZ-2D R/B passes over latitudes between 59.9°N and 59.9°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,221 active satellites in total, of which 85 share a similar altitude band with CZ-2D 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-2D R/B orbits in Low Earth Orbit (LEO) at altitudes between 763 km (perigee) and 792 km (apogee), with an average altitude of approximately 778 km. It completes one orbit every 100 minutes, travelling at approximately 26,882 km/h (16,704 mph).
CZ-2D R/B (NORAD ID 54215) 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-2D R/B was launched on 2022-10-29 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-2D R/B (NORAD ID 54215) 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-2D R/B travels at approximately 26,882 km/h (16,704 mph) — roughly 7.47 km/s. It completes 14.34 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.