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YZ-1 R/B

NORAD 44544 Rocket Body MEO 2019-061C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
22023 km
Apogee
22223 km
Inclination
54.4°
Period
798.1 min
Mean Motion
1.80432615 rev/day
TLE Epoch
2026-06-23 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude22,123 km
Orbital Velocity13,465 km/h
Velocity3.74 km/s
Orbital Period13 hours 18 minutes
Orbits / Day1.80
Eccentricity0.0035
Semi-Major Axis28,494 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2019-09-22
Launch Site
Xichang, China
Int'l Designator
2019-061C
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 2019-09-22 from Xichang, China on the Beidou-3 M23/M24 launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 22,023 km and 22,223 km with an inclination of 54.4°. It travels at approximately 13,465 km/h (3.74 km/s), completing one full orbit every 13 hours 18 minutes — that’s roughly 1.80 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 22,123 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 10 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 54.4°, YZ-1 R/B passes over latitudes between 54.4°N and 54.4°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 22,023 km (perigee) and 22,223 km (apogee), with an average altitude of approximately 22,123 km. It completes one orbit every 13 hours 18 minutes, travelling at approximately 13,465 km/h (8,367 mph).
YZ-1 R/B (NORAD ID 44544) 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 2019-09-22 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks YZ-1 R/B (NORAD ID 44544) 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 13,465 km/h (8,367 mph) — roughly 3.74 km/s. It completes 1.80 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.