GAOFEN 9 DEB
NORAD 44600
Debris
LEO
2015-047B
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LEO · NORAD 44600
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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
583 km
Apogee
800 km
Inclination
98.1°
Period
98.6 min
Mean Motion
14.60499101 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude692 km
Orbital Velocity27,045 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.60
Eccentricity0.0154
Semi-Major Axis7,063 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 CNSA (China)
Launch Date
2015-09-14
Launch Site
Jiuquan, China
Int'l Designator
2015-047B
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
GAOFEN 9 DEB is a tracked piece of space debris attributed to China, launched on 2015-09-14 from Jiuquan, China on the GF-9 launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 583 km and 800 km with an inclination of 98.1°. It travels at approximately 27,045 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.60 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 ~10–25 years. As orbital debris, GAOFEN 9 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 9 DEB orbits at an average altitude of 692 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 9 DEB’s average altitude, there are currently 286 active payloads and 1,349 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.1°, GAOFEN 9 DEB passes over latitudes between 98.1°N and 98.1°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 58 share a similar altitude band with GAOFEN 9 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 9 DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 692 km altitude. Its 98.1° 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 99 minutes, travelling at 27,045 km/h.
GAOFEN 9 DEB (NORAD ID 44600) 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 9 DEB was launched on 2015-09-14 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks GAOFEN 9 DEB (NORAD ID 44600) 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 9 DEB travels at approximately 27,045 km/h (16,805 mph) — roughly 7.51 km/s. It completes 14.60 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 7.51 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 9 DEB. Read more about debris statistics and the Kessler syndrome.