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CZ-2C R/B

NORAD 48862 Rocket Body LEO 2021-055C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
555 km
Apogee
650 km
Inclination
35.1°
Period
96.8 min
Mean Motion
14.88434282 rev/day
TLE Epoch
2026-06-25 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude603 km
Orbital Velocity27,217 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.88
Eccentricity0.0068
Semi-Major Axis6,974 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2021-06-18
Launch Site
Xichang, China
Int'l Designator
2021-055C
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 2021-06-18 from Xichang, China on the YG-30-09 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 555 km and 650 km with an inclination of 35.1°. It travels at approximately 27,217 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.88 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 603 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 1,631 active payloads and 673 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 9.3% of all active satellites. With an inclination of 35.1°, CZ-2C R/B passes over latitudes between 35.1°N and 35.1°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 174 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 555 km (perigee) and 650 km (apogee), with an average altitude of approximately 603 km. It completes one orbit every 97 minutes, travelling at approximately 27,217 km/h (16,912 mph).
CZ-2C R/B (NORAD ID 48862) 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 2021-06-18 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 48862) 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 27,217 km/h (16,912 mph) — roughly 7.56 km/s. It completes 14.88 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.