Skip to content
Home Library Satellite Directory CZ-2C R/B

CZ-2C R/B

NORAD 58916 Rocket Body LEO 2024-023M
CONNECTING… LEO · NORAD 58916
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
590 km
Apogee
723 km
Inclination
49.9°
Period
97.9 min
Mean Motion
14.71438053 rev/day
TLE Epoch
2026-06-25 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude657 km
Orbital Velocity27,113 km/h
Velocity7.53 km/s
Orbital Period98 minutes
Orbits / Day14.71
Eccentricity0.0095
Semi-Major Axis7,028 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2024-02-02
Launch Site
Xichang, China
Int'l Designator
2024-023M
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 2024-02-02 from Xichang, China on the GeeSat launch. It orbits in Low Earth Orbit (LEO) at altitudes between 590 km and 723 km with an inclination of 49.9°. It travels at approximately 27,113 km/h (7.53 km/s), completing one full orbit every 98 minutes — that’s roughly 14.71 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. 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 657 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-2C R/B’s average altitude, there are currently 679 active payloads and 1,105 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 49.9°, CZ-2C R/B passes over latitudes between 49.9°N and 49.9°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 149 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 590 km (perigee) and 723 km (apogee), with an average altitude of approximately 657 km. It completes one orbit every 98 minutes, travelling at approximately 27,113 km/h (16,847 mph).
CZ-2C R/B (NORAD ID 58916) 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 2024-02-02 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-2C R/B (NORAD ID 58916) 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 27,113 km/h (16,847 mph) — roughly 7.53 km/s. It completes 14.71 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.