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YZ-1 R/B

NORAD 40751 Rocket Body MEO 2015-037D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
21741 km
Apogee
28152 km
Inclination
56.4°
Period
919.6 min
Mean Motion
1.56591386 rev/day
TLE Epoch
2026-06-25 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude24,947 km
Orbital Velocity12,843 km/h
Velocity3.57 km/s
Orbital Period15 hours 20 minutes
Orbits / Day1.57
Eccentricity0.1024
Semi-Major Axis31,318 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2015-07-25
Launch Site
Xichang, China
Int'l Designator
2015-037D
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 2015-07-25 from Xichang, China on the Beidou M1S?M2S launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 21,741 km and 28,152 km with an inclination of 56.4°. It travels at approximately 12,843 km/h (3.57 km/s), completing one full orbit every 15 hours 20 minutes — that’s roughly 1.57 orbits per day. Its orbital eccentricity of 0.1024 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 24,947 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. With an inclination of 56.4°, YZ-1 R/B passes over latitudes between 56.4°N and 56.4°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 21,741 km (perigee) and 28,152 km (apogee), with an average altitude of approximately 24,947 km. It completes one orbit every 15 hours 20 minutes, travelling at approximately 12,843 km/h (7,980 mph).
YZ-1 R/B (NORAD ID 40751) 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 2015-07-25 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks YZ-1 R/B (NORAD ID 40751) 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 12,843 km/h (7,980 mph) — roughly 3.57 km/s. It completes 1.57 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 3 sunrises and sunsets every 24 hours.