YZ-2 R/B
NORAD 41840
Rocket Body
GEO
2016-065C
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GEO · NORAD 41840
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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
35758 km
Apogee
39856 km
Inclination
9.4°
Period
1540.5 min
Mean Motion
0.93474303 rev/day
TLE Epoch
2026-06-24 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,807 km
Orbital Velocity10,814 km/h
Velocity3.00 km/s
Orbital Period25.7 hours
Orbits / Day0.93
Eccentricity0.0464
Semi-Major Axis44,178 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2016-11-03
Launch Site
Wenchang, China
Int'l Designator
2016-065C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
YZ-2 R/B is a spent rocket body associated with China, launched on 2016-11-03 from Wenchang, China on the SJ-17 launch. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,758 km and 39,856 km with an inclination of 9.4°. It travels at approximately 10,814 km/h (3.00 km/s), completing one full orbit every 25.7 hours — that’s roughly 0.93 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Spent rocket bodies like YZ-2 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-2 R/B occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 9.4°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. 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-2 R/B orbits at approximately 37,807 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 10,814 km/h — it just keeps pace with the ground below. With an inclination of 9.4°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
YZ-2 R/B (NORAD ID 41840) 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-2 R/B was launched on 2016-11-03 from Wenchang, China, China’s newest coastal launch facility on Hainan Island, used for heavy-lift Long March 5 missions. View the full satellite launch log.
Yes — Orbital Radar tracks YZ-2 R/B (NORAD ID 41840) 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-2 R/B travels at approximately 10,814 km/h (6,719 mph) — roughly 3.00 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.