Skip to content
Home Library Satellite Directory YAOGAN 4 DEB

YAOGAN 4 DEB

NORAD 35575 Debris LEO 2008-061B
CONNECTING… LEO · NORAD 35575
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
628 km
Apogee
927 km
Inclination
97.8°
Period
100.4 min
Mean Motion
14.34230628 rev/day
TLE Epoch
2026-06-18 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude778 km
Orbital Velocity26,882 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.34
Eccentricity0.0209
Semi-Major Axis7,149 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2008-12-01
Launch Site
Jiuquan, China
Int'l Designator
2008-061B
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
YAOGAN 4 DEB is a tracked piece of space debris attributed to China, launched on 2008-12-01 from Jiuquan, China. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 628 km and 927 km with an inclination of 97.8°. It travels at approximately 26,882 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.34 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, YAOGAN 4 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 4 DEB orbits at an average altitude of 778 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of YAOGAN 4 DEB’s average altitude, there are currently 417 active payloads and 2,160 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 97.8°, YAOGAN 4 DEB passes over latitudes between 97.8°N and 97.8°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 1,218 active satellites in total, of which 83 share a similar altitude band with YAOGAN 4 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 4 DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 778 km altitude. Its 97.8° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 100 minutes, travelling at 26,882 km/h.
YAOGAN 4 DEB (NORAD ID 35575) 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 4 DEB was launched on 2008-12-01 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN 4 DEB (NORAD ID 35575) 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 4 DEB travels at approximately 26,882 km/h (16,704 mph) — roughly 7.47 km/s. It completes 14.34 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.47 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 4 DEB. Read more about debris statistics and the Kessler syndrome.