CZ-3B R/B
NORAD 59707
Rocket Body
LEO
2024-087C
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LEO · NORAD 59707
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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
132 km
Apogee
906 km
Inclination
53.0°
Period
95.0 min
Mean Motion
15.20283751 rev/day
TLE Epoch
2026-06-25 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude519 km
Orbital Velocity27,382 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.20
Eccentricity0.0562
Semi-Major Axis6,890 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2024-05-09
Launch Site
Xichang, China
Int'l Designator
2024-087C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-3B R/B is a spent rocket body associated with China, launched on 2024-05-09 from Xichang, China on the Zhuhui Tianwang 1-01 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 132 km and 906 km with an inclination of 53.0°. It travels at approximately 27,382 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.20 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Spent rocket bodies like CZ-3B 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-3B R/B orbits at an average altitude of 519 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-3B R/B’s average altitude, there are currently 7,642 active payloads and 272 tracked debris or rocket body fragments — notable neighbours include STARLINK-1039, STARLINK-1184, STARLINK-1231. This makes it one of the more crowded altitude bands, containing roughly 43.7% of all active satellites. With an inclination of 53.0°, CZ-3B R/B passes over latitudes between 53.0°N and 53.0°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 219 share a similar altitude band with CZ-3B 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-3B R/B orbits in Low Earth Orbit (LEO) at altitudes between 132 km (perigee) and 906 km (apogee), with an average altitude of approximately 519 km. It completes one orbit every 95 minutes, travelling at approximately 27,382 km/h (17,014 mph).
CZ-3B R/B (NORAD ID 59707) 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-3B R/B was launched on 2024-05-09 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-3B R/B (NORAD ID 59707) 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-3B R/B travels at approximately 27,382 km/h (17,014 mph) — roughly 7.61 km/s. It completes 15.20 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.