CZ-2C R/B
NORAD 55846
Rocket Body
LEO
2023-032C
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LEO · NORAD 55846
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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
407 km
Apogee
445 km
Inclination
97.6°
Period
93.1 min
Mean Motion
15.46752991 rev/day
TLE Epoch
2026-10-15 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude426 km
Orbital Velocity27,568 km/h
Velocity7.66 km/s
Orbital Period93 minutes
Orbits / Day15.47
Eccentricity0.0028
Semi-Major Axis6,797 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2023-03-13
Launch Site
Jiuquan Satellite Launch Center, China
Int'l Designator
2023-032C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-2C R/B is a spent rocket body associated with China, launched on 2023-03-13 from Jiuquan Satellite Launch Center, China on the Horus 2 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 407 km and 445 km with an inclination of 97.6°. It travels at approximately 27,568 km/h (7.66 km/s), completing one full orbit every 93 minutes — that’s roughly 15.47 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 ~1–3 years. Spent rocket bodies like CZ-2C 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-2C R/B orbits at an average altitude of 426 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-2C R/B’s average altitude, there are currently 6,786 active payloads and 119 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1017, STARLINK-1039. This makes it one of the more crowded altitude bands, containing roughly 36% of all active satellites. With an inclination of 97.6°, CZ-2C R/B passes over latitudes between 97.6°N and 97.6°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 1,323 active satellites in total, of which 70 share a similar altitude band with CZ-2C 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-2C R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 426 km altitude. Its 97.6° 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 93 minutes, travelling at 27,568 km/h.
CZ-2C R/B (NORAD ID 55846) 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-2C R/B was launched on 2023-03-13 from Jiuquan Satellite Launch Center, 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-2C R/B (NORAD ID 55846) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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-2C R/B travels at approximately 27,568 km/h (17,130 mph) — roughly 7.66 km/s. It completes 15.47 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.