CZ-4B R/B
NORAD 100657
Rocket Body
LEO
2026-205G
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LEO · NORAD 100657
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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
300 km
Apogee
518 km
Inclination
45.1°
Period
92.8 min
Mean Motion
15.52616181 rev/day
TLE Epoch
2026-09-11 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude409 km
Orbital Velocity27,603 km/h
Velocity7.67 km/s
Orbital Period93 minutes
Orbits / Day15.53
Eccentricity0.0161
Semi-Major Axis6,780 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-09-10
Launch Site
Jiuquan, China
Int'l Designator
2026-205G
Object Type
Rocket Body
RCS Size
Unknown
📖 About This Object
CZ-4B R/B is a spent rocket body associated with China, launched on 2026-09-10 from Jiuquan, China. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 300 km and 518 km with an inclination of 45.1°. It travels at approximately 27,603 km/h (7.67 km/s), completing one full orbit every 93 minutes — that’s roughly 15.53 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Spent rocket bodies like CZ-4B 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-4B R/B orbits at an average altitude of 409 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-4B R/B’s average altitude, there are currently 974 active payloads and 102 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1008, STARLINK-1012. This makes it one of the more crowded altitude bands, containing roughly 5.4% of all active satellites. With an inclination of 45.1°, CZ-4B R/B passes over latitudes between 45.1°N and 45.1°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 1,272 active satellites in total, of which 50 share a similar altitude band with CZ-4B 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-4B R/B orbits in Low Earth Orbit (LEO) at altitudes between 300 km (perigee) and 518 km (apogee), with an average altitude of approximately 409 km. It completes one orbit every 93 minutes, travelling at approximately 27,603 km/h (17,152 mph).
CZ-4B R/B (NORAD ID 100657) 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-4B R/B was launched on 2026-09-10 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4B R/B (NORAD ID 100657) 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-4B R/B travels at approximately 27,603 km/h (17,152 mph) — roughly 7.67 km/s. It completes 15.53 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.