YZ-1 R/B
NORAD 58656
Rocket Body
MEO
2023-207C
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MEO · NORAD 58656
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Altitude (km)
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🛰️ Orbital Parameters
Perigee
22170 km
Apogee
22322 km
Inclination
55.8°
Period
803.3 min
Mean Motion
1.79266145 rev/day
TLE Epoch
2026-06-24 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude22,246 km
Orbital Velocity13,436 km/h
Velocity3.73 km/s
Orbital Period13 hours 23 minutes
Orbits / Day1.79
Eccentricity0.0027
Semi-Major Axis28,617 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2023-12-26
Launch Site
Xichang, China
Int'l Designator
2023-207C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
YZ-1 R/B is a spent rocket body associated with China, launched on 2023-12-26 from Xichang, China on the Beidou launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 22,170 km and 22,322 km with an inclination of 55.8°. It travels at approximately 13,436 km/h (3.73 km/s), completing one full orbit every 13 hours 23 minutes — that’s roughly 1.79 orbits per day. Spent rocket bodies like YZ-1 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
YZ-1 R/B orbits at an average altitude of 22,246 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 YZ-1 R/B’s average altitude, there are currently 0 active payloads and 12 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 55.8°, YZ-1 R/B passes over latitudes between 55.8°N and 55.8°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. 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
YZ-1 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 22,170 km (perigee) and 22,322 km (apogee), with an average altitude of approximately 22,246 km. It completes one orbit every 13 hours 23 minutes, travelling at approximately 13,436 km/h (8,349 mph).
YZ-1 R/B (NORAD ID 58656) 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.
YZ-1 R/B was launched on 2023-12-26 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks YZ-1 R/B (NORAD ID 58656) 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.
YZ-1 R/B travels at approximately 13,436 km/h (8,349 mph) — roughly 3.73 km/s. It completes 1.79 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.