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YAOGAN 25C DEB

NORAD 69732 Debris LEO 2014-080M
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
740 km
Apogee
1220 km
Inclination
63.4°
Period
104.7 min
Mean Motion
13.75504833 rev/day
TLE Epoch
2026-07-26 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude980 km
Orbital Velocity26,509 km/h
Velocity7.36 km/s
Orbital Period105 minutes
Orbits / Day13.76
Eccentricity0.0326
Semi-Major Axis7,351 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2014-12-10
Launch Site
Jiuquan, China
Int'l Designator
2014-080M
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 740 km and 1,220 km with an inclination of 63.4°. It travels at approximately 26,509 km/h (7.36 km/s), completing one full orbit every 105 minutes — that’s roughly 13.76 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 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 980 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 317 active payloads and 962 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 62 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 740 km (perigee) and 1,220 km (apogee), with an average altitude of approximately 980 km. It completes one orbit every 105 minutes, travelling at approximately 26,509 km/h (16,472 mph).
YAOGAN 25C DEB (NORAD ID 69732) 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN 25C DEB (NORAD ID 69732) 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 26,509 km/h (16,472 mph) — roughly 7.36 km/s. It completes 13.76 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 7.36 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.