YAOGAN 25C DEB
NORAD 69731
Debris
LEO
2014-080L
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LEO · NORAD 69731
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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
768 km
Apogee
1271 km
Inclination
63.4°
Period
105.5 min
Mean Motion
13.64482587 rev/day
TLE Epoch
2026-07-27 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,020 km
Orbital Velocity26,438 km/h
Velocity7.34 km/s
Orbital Period106 minutes
Orbits / Day13.64
Eccentricity0.0340
Semi-Major Axis7,391 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2014-12-10
Launch Site
Jiuquan, China
Int'l Designator
2014-080L
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
YAOGAN 25C DEB is a tracked piece of space debris attributed to China, launched on 2014-12-10 from Jiuquan, China on the YG-25 launch. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 768 km and 1,271 km with an inclination of 63.4°. It travels at approximately 26,438 km/h (7.34 km/s), completing one full orbit every 106 minutes — that’s roughly 13.64 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. As orbital debris, YAOGAN 25C 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 25C DEB orbits at an average altitude of 1,020 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 25C DEB’s average altitude, there are currently 338 active payloads and 739 tracked debris or rocket body fragments. With an inclination of 63.4°, YAOGAN 25C DEB passes over latitudes between 63.4°N and 63.4°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,245 active satellites in total, of which 174 share a similar altitude band with YAOGAN 25C 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 25C DEB orbits in Low Earth Orbit (LEO) at altitudes between 768 km (perigee) and 1,271 km (apogee), with an average altitude of approximately 1,020 km. It completes one orbit every 106 minutes, travelling at approximately 26,438 km/h (16,428 mph).
YAOGAN 25C DEB (NORAD ID 69731) 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 25C DEB was launched on 2014-12-10 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN 25C DEB (NORAD ID 69731) 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 25C DEB travels at approximately 26,438 km/h (16,428 mph) — roughly 7.34 km/s. It completes 13.64 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.34 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 25C DEB. Read more about debris statistics and the Kessler syndrome.