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CZ-3B R/B

NORAD 42663 Rocket Body MEO 2017-018B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
220 km
Apogee
27414 km
Inclination
20.4°
Period
476.0 min
Mean Motion
3.02498984 rev/day
TLE Epoch
2026-06-24 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude13,817 km
Orbital Velocity15,996 km/h
Velocity4.44 km/s
Orbital Period7 hours 56 minutes
Orbits / Day3.02
Eccentricity0.6735
Semi-Major Axis20,188 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2017-04-12
Launch Site
Xichang, China
Int'l Designator
2017-018B
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 2017-04-12 from Xichang, China on the Shi Jian 13 launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 220 km and 27,414 km with an inclination of 20.4°. It travels at approximately 15,996 km/h (4.44 km/s), completing one full orbit every 7 hours 56 minutes — that’s roughly 3.02 orbits per day. Its orbital eccentricity of 0.6735 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 13,817 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of CZ-3B R/B’s average altitude, there are currently 0 active payloads and 9 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 20.4°, CZ-3B R/B passes over latitudes between 20.4°N and 20.4°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.
🔗 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 Medium Earth Orbit (MEO) at altitudes between 220 km (perigee) and 27,414 km (apogee), with an average altitude of approximately 13,817 km. It completes one orbit every 7 hours 56 minutes, travelling at approximately 15,996 km/h (9,940 mph).
CZ-3B R/B (NORAD ID 42663) 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 2017-04-12 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-3B R/B (NORAD ID 42663) 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 15,996 km/h (9,940 mph) — roughly 4.44 km/s. It completes 3.02 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 6 sunrises and sunsets every 24 hours.