YAOGAN 9B DEB
NORAD 38303
Debris
LEO
2010-009G
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LEO · NORAD 38303
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
578 km
Apogee
1257 km
Inclination
63.3°
Period
103.4 min
Mean Motion
13.93060356 rev/day
TLE Epoch
2026-07-30 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude918 km
Orbital Velocity26,623 km/h
Velocity7.40 km/s
Orbital Period103 minutes
Orbits / Day13.93
Eccentricity0.0466
Semi-Major Axis7,289 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2010-03-05
Launch Site
Jiuquan, China
Int'l Designator
2010-009G
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
YAOGAN 9B DEB is a tracked piece of space debris attributed to China, launched on 2010-03-05 from Jiuquan, China on the yaogan weixing jiuhao launch. After 16 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 578 km and 1,257 km with an inclination of 63.3°. It travels at approximately 26,623 km/h (7.40 km/s), completing one full orbit every 103 minutes — that’s roughly 13.93 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, YAOGAN 9B 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 9B DEB orbits at an average altitude of 918 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 9B DEB’s average altitude, there are currently 210 active payloads and 1,164 tracked debris or rocket body fragments. With an inclination of 63.3°, YAOGAN 9B DEB passes over latitudes between 63.3°N and 63.3°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,248 active satellites in total, of which 49 share a similar altitude band with YAOGAN 9B 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 9B DEB orbits in Low Earth Orbit (LEO) at altitudes between 578 km (perigee) and 1,257 km (apogee), with an average altitude of approximately 918 km. It completes one orbit every 103 minutes, travelling at approximately 26,623 km/h (16,543 mph).
YAOGAN 9B DEB (NORAD ID 38303) 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 9B DEB was launched on 2010-03-05 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN 9B DEB (NORAD ID 38303) 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 9B DEB travels at approximately 26,623 km/h (16,543 mph) — roughly 7.40 km/s. It completes 13.93 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 7.40 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 9B DEB. Read more about debris statistics and the Kessler syndrome.