YAOGAN-50 02 DEB
NORAD 100806
Debris
LEO
2026-051BA
CONNECTING…
LEO · NORAD 100806
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
789 km
Apogee
968 km
Inclination
142.0°
Period
102.5 min
Mean Motion
14.04520966 rev/day
TLE Epoch
2026-10-21 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude879 km
Orbital Velocity26,694 km/h
Velocity7.42 km/s
Orbital Period103 minutes
Orbits / Day14.05
Eccentricity0.0123
Semi-Major Axis7,250 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
2026-051BA
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 789 km and 968 km with an inclination of 142.0°. It travels at approximately 26,694 km/h (7.42 km/s), completing one full orbit every 103 minutes — that’s roughly 14.05 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 879 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 242 active payloads and 1,937 tracked debris or rocket body fragments. With an inclination of 142.0°, YAOGAN-50 02 DEB passes over latitudes between 142.0°N and 142.0°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 1,341 active satellites in total, of which 87 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 789 km (perigee) and 968 km (apogee), with an average altitude of approximately 879 km. It completes one orbit every 103 minutes, travelling at approximately 26,694 km/h (16,587 mph).
YAOGAN-50 02 DEB (NORAD ID 100806) 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 100806) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 26,694 km/h (16,587 mph) — roughly 7.42 km/s. It completes 14.05 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 7.42 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.