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FENGYUN 1C DEB

NORAD 31820 Debris LEO 1999-025CHJ
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
478 km
Apogee
666 km
Inclination
99.0°
Period
96.1 min
Mean Motion
14.98268278 rev/day
TLE Epoch
2026-06-24 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude572 km
Orbital Velocity27,277 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.98
Eccentricity0.0135
Semi-Major Axis6,943 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
1999-05-10
Launch Site
Taiyuan, China
Int'l Designator
1999-025CHJ
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
FENGYUN 1C DEB is a tracked piece of space debris attributed to China, launched on 1999-05-10 from Taiyuan, China on the Feng Yun Yi Beng launch. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 478 km and 666 km with an inclination of 99.0°. It travels at approximately 27,277 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 14.98 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 ~3–10 years. As orbital debris, FENGYUN 1C 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
FENGYUN 1C DEB orbits at an average altitude of 572 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 FENGYUN 1C DEB’s average altitude, there are currently 2,971 active payloads and 500 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-1522, STARLINK-2112. This makes it one of the more crowded altitude bands, containing roughly 17% of all active satellites. With an inclination of 99.0°, FENGYUN 1C DEB passes over latitudes between 99.0°N and 99.0°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 1,221 active satellites in total, of which 172 share a similar altitude band with FENGYUN 1C DEB.
🔗 Fengyun-1C ASAT Debris

This debris object was created by China's kinetic-kill anti-satellite test on 11 January 2007, which destroyed the Fengyun-1C weather satellite at approximately 865 km altitude. The test generated over 3,500 trackable fragments — the worst debris event in spaceflight history — with debris expected to persist in orbit for decades to centuries due to the high altitude. About 2,800 fragments remain catalogued as of 2026.

❓ Frequently Asked Questions
FENGYUN 1C DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 572 km altitude. Its 99.0° 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 96 minutes, travelling at 27,277 km/h.
FENGYUN 1C DEB (NORAD ID 31820) 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.
FENGYUN 1C DEB was launched on 1999-05-10 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 1C DEB (NORAD ID 31820) 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.
FENGYUN 1C DEB travels at approximately 27,277 km/h (16,949 mph) — roughly 7.58 km/s. It completes 14.98 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 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 7.58 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 FENGYUN 1C DEB. Read more about debris statistics and the Kessler syndrome.