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CZ-4C R/B

NORAD 65816 Rocket Body LEO 2025-219B
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🛰️ Orbital Parameters
Perigee
631 km
Apogee
800 km
Inclination
98.7°
Period
99.1 min
Mean Motion
14.53122745 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude716 km
Orbital Velocity26,999 km/h
Velocity7.50 km/s
Orbital Period99 minutes
Orbits / Day14.53
Eccentricity0.0119
Semi-Major Axis7,087 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-09-26
Launch Site
Jiuquan, China
Int'l Designator
2025-219B
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 2025-09-26 from Jiuquan, China on the FY3-08 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 631 km and 800 km with an inclination of 98.7°. It travels at approximately 26,999 km/h (7.50 km/s), completing one full orbit every 99 minutes — that’s roughly 14.53 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 ~25–100 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 716 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 278 active payloads and 1,651 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.7°, CZ-4C R/B passes over latitudes between 98.7°N and 98.7°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 59 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 716 km altitude. Its 98.7° 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 99 minutes, travelling at 26,999 km/h.
CZ-4C R/B (NORAD ID 65816) 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 2025-09-26 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4C R/B (NORAD ID 65816) 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 26,999 km/h (16,777 mph) — roughly 7.50 km/s. It completes 14.53 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.