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YAOGAN-50 02 DEB

NORAD 100589 Debris LEO 2026-051AD
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
793 km
Apogee
976 km
Inclination
141.9°
Period
102.7 min
Mean Motion
14.03304849 rev/day
TLE Epoch
2026-09-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude885 km
Orbital Velocity26,683 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.03
Eccentricity0.0126
Semi-Major Axis7,256 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2026-03-15
Launch Site
Taiyuan Satellite Launch Center, China
Int'l Designator
2026-051AD
Object Type
Debris
RCS Size
Unknown
📖 About This Object
YAOGAN-50 02 DEB is a tracked piece of space debris attributed to China, launched on 2026-03-15 from Taiyuan Satellite Launch Center, China on the YG50-02 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 793 km and 976 km with an inclination of 141.9°. It travels at approximately 26,683 km/h (7.41 km/s), completing one full orbit every 103 minutes — that’s roughly 14.03 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, YAOGAN-50 02 DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
YAOGAN-50 02 DEB orbits at an average altitude of 885 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of YAOGAN-50 02 DEB’s average altitude, there are currently 237 active payloads and 1,818 tracked debris or rocket body fragments. With an inclination of 141.9°, YAOGAN-50 02 DEB passes over latitudes between 141.9°N and 141.9°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 1,288 active satellites in total, of which 80 share a similar altitude band with YAOGAN-50 02 DEB.
🔗 Yaogan Reconnaissance Series

This satellite is part of China's Yaogan series, officially described as “remote sensing” satellites but widely assessed by analysts to serve military reconnaissance, signals intelligence and ocean surveillance missions. The series includes optical imaging, synthetic aperture radar (SAR) and electronic intelligence (ELINT) variants, some operating in coordinated orbital formations for persistent maritime monitoring.

❓ Frequently Asked Questions
YAOGAN-50 02 DEB orbits in Low Earth Orbit (LEO) at altitudes between 793 km (perigee) and 976 km (apogee), with an average altitude of approximately 885 km. It completes one orbit every 103 minutes, travelling at approximately 26,683 km/h (16,580 mph).
YAOGAN-50 02 DEB (NORAD ID 100589) is a piece of tracked orbital debris attributed to China. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
YAOGAN-50 02 DEB was launched on 2026-03-15 from Taiyuan Satellite Launch Center, China. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN-50 02 DEB (NORAD ID 100589) 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.
YAOGAN-50 02 DEB travels at approximately 26,683 km/h (16,580 mph) — roughly 7.41 km/s. It completes 14.03 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.41 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like YAOGAN-50 02 DEB. Read more about debris statistics and the Kessler syndrome.