CZ-4C R/B
NORAD 43462
Rocket Body
LEO
2018-043B
CONNECTING…
LEO · NORAD 43462
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
547 km
Apogee
667 km
Inclination
98.2°
Period
96.8 min
Mean Motion
14.87107005 rev/day
TLE Epoch
2026-06-26 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude607 km
Orbital Velocity27,209 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.87
Eccentricity0.0086
Semi-Major Axis6,978 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2018-05-08
Launch Site
Taiyuan, China
Int'l Designator
2018-043B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-4C R/B is a spent rocket body associated with China, launched on 2018-05-08 from Taiyuan, China on the Gao Fen 5 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 547 km and 667 km with an inclination of 98.2°. It travels at approximately 27,209 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.87 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Spent rocket bodies like CZ-4C 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-4C R/B orbits at an average altitude of 607 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of CZ-4C R/B’s average altitude, there are currently 1,637 active payloads and 691 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 9.4% of all active satellites. With an inclination of 98.2°, CZ-4C R/B passes over latitudes between 98.2°N and 98.2°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. China operates approximately 1,221 active satellites in total, of which 173 share a similar altitude band with CZ-4C 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-4C R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 607 km altitude. Its 98.2° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 97 minutes, travelling at 27,209 km/h.
CZ-4C R/B (NORAD ID 43462) 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-4C R/B was launched on 2018-05-08 from Taiyuan, 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-4C R/B (NORAD ID 43462) 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-4C R/B travels at approximately 27,209 km/h (16,907 mph) — roughly 7.56 km/s. It completes 14.87 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.