CZ-2C R/B
NORAD 58754
Rocket Body
LEO
2024-007B
CONNECTING…
LEO · NORAD 58754
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
386 km
Apogee
464 km
Inclination
29.0°
Period
93.1 min
Mean Motion
15.47086249 rev/day
TLE Epoch
2026-10-15 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude425 km
Orbital Velocity27,571 km/h
Velocity7.66 km/s
Orbital Period93 minutes
Orbits / Day15.47
Eccentricity0.0057
Semi-Major Axis6,796 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2024-01-09
Launch Site
Xichang Satellite Launch Center, China
Int'l Designator
2024-007B
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 2024-01-09 from Xichang Satellite Launch Center, China on the Einstein Probe launch. It orbits in Low Earth Orbit (LEO) at altitudes between 386 km and 464 km with an inclination of 29.0°. It travels at approximately 27,571 km/h (7.66 km/s), completing one full orbit every 93 minutes — that’s roughly 15.47 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 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 425 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of CZ-2C R/B’s average altitude, there are currently 6,759 active payloads and 118 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1017, STARLINK-1039. This makes it one of the more crowded altitude bands, containing roughly 36.2% of all active satellites. With an inclination of 29.0°, CZ-2C R/B passes over latitudes between 29.0°N and 29.0°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 1,321 active satellites in total, of which 69 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 386 km (perigee) and 464 km (apogee), with an average altitude of approximately 425 km. It completes one orbit every 93 minutes, travelling at approximately 27,571 km/h (17,132 mph).
CZ-2C R/B (NORAD ID 58754) 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 2024-01-09 from Xichang Satellite Launch Center, China. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-2C R/B (NORAD ID 58754) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 27,571 km/h (17,132 mph) — roughly 7.66 km/s. It completes 15.47 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.