GAOFEN 3 DEB
NORAD 42679
Debris
LEO
2016-049D
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LEO · NORAD 42679
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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
732 km
Apogee
741 km
Inclination
98.3°
Period
99.5 min
Mean Motion
14.46661386 rev/day
TLE Epoch
2026-06-20 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude737 km
Orbital Velocity26,960 km/h
Velocity7.49 km/s
Orbital Period100 minutes
Orbits / Day14.47
Eccentricity0.0006
Semi-Major Axis7,108 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 CNSA (China)
Launch Date
2016-08-09
Launch Site
Taiyuan, China
Int'l Designator
2016-049D
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
GAOFEN 3 DEB is a tracked piece of space debris attributed to China, launched on 2016-08-09 from Taiyuan, China on the Gaofen 3 launch. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 732 km and 741 km with an inclination of 98.3°. It travels at approximately 26,960 km/h (7.49 km/s), completing one full orbit every 100 minutes — that’s roughly 14.47 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, GAOFEN 3 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
GAOFEN 3 DEB orbits at an average altitude of 737 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 GAOFEN 3 DEB’s average altitude, there are currently 362 active payloads and 1,859 tracked debris or rocket body fragments — notable neighbours include TERRA, LANDSAT 9. With an inclination of 98.3°, GAOFEN 3 DEB passes over latitudes between 98.3°N and 98.3°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 41 share a similar altitude band with GAOFEN 3 DEB.
🔗 Gaofen High-Resolution Imaging
This satellite is part of China's Gaofen high-resolution Earth observation programme, part of the China High-resolution Earth Observation System (CHEOS). Gaofen satellites provide sub-metre optical and radar imagery for agriculture, disaster monitoring, urban planning and environmental surveillance.
❓ Frequently Asked Questions
GAOFEN 3 DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 737 km altitude. Its 98.3° 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 26,960 km/h.
GAOFEN 3 DEB (NORAD ID 42679) 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.
GAOFEN 3 DEB was launched on 2016-08-09 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks GAOFEN 3 DEB (NORAD ID 42679) 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.
GAOFEN 3 DEB travels at approximately 26,960 km/h (16,752 mph) — roughly 7.49 km/s. It completes 14.47 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 7.49 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 GAOFEN 3 DEB. Read more about debris statistics and the Kessler syndrome.