CZ-2C R/B
NORAD 52794
Rocket Body
LEO
2022-058K
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LEO · NORAD 52794
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
359 km
Apogee
402 km
Inclination
50.2°
Period
92.2 min
Mean Motion
15.62450808 rev/day
TLE Epoch
2026-06-26 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude381 km
Orbital Velocity27,661 km/h
Velocity7.68 km/s
Orbital Period92 minutes
Orbits / Day15.62
Eccentricity0.0032
Semi-Major Axis6,752 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2022-06-02
Launch Site
Xichang, China
Int'l Designator
2022-058K
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-2C R/B is a spent rocket body associated with China, launched on 2022-06-02 from Xichang, China on the GeeSat 01-01/09 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 359 km and 402 km with an inclination of 50.2°. It travels at approximately 27,661 km/h (7.68 km/s), completing one full orbit every 92 minutes — that’s roughly 15.62 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Spent rocket bodies like CZ-2C 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-2C R/B orbits at an average altitude of 381 km in the lower reaches of Low Earth Orbit, where atmospheric drag is significant and orbital lifetimes are measured in months to a few years. This is the busiest corridor in space — home to crewed spacecraft, rapid-revisit imaging satellites and the densest part of the Starlink constellation. Within ±50 km of CZ-2C R/B’s average altitude, there are currently 1,280 active payloads and 62 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 7.3% of all active satellites. With an inclination of 50.2°, CZ-2C R/B passes over latitudes between 50.2°N and 50.2°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 37 share a similar altitude band with CZ-2C 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-2C R/B orbits in Low Earth Orbit (LEO) at altitudes between 359 km (perigee) and 402 km (apogee), with an average altitude of approximately 381 km. It completes one orbit every 92 minutes, travelling at approximately 27,661 km/h (17,188 mph).
CZ-2C R/B (NORAD ID 52794) 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-2C R/B was launched on 2022-06-02 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-2C R/B (NORAD ID 52794) 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-2C R/B travels at approximately 27,661 km/h (17,188 mph) — roughly 7.68 km/s. It completes 15.62 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.