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FENGYUN 1C DEB

NORAD 32203 Debris LEO 1999-025CUZ
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
324 km
Apogee
463 km
Inclination
97.0°
Period
92.4 min
Mean Motion
15.58027365 rev/day
TLE Epoch
2026-06-25 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude394 km
Orbital Velocity27,635 km/h
Velocity7.68 km/s
Orbital Period92 minutes
Orbits / Day15.58
Eccentricity0.0103
Semi-Major Axis6,765 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
1999-05-10
Launch Site
Taiyuan, China
Int'l Designator
1999-025CUZ
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 324 km and 463 km with an inclination of 97.0°. It travels at approximately 27,635 km/h (7.68 km/s), completing one full orbit every 92 minutes — that’s roughly 15.58 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 months to ~1 year. 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 394 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 1,306 active payloads and 84 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 7.5% of all active satellites. With an inclination of 97.0°, FENGYUN 1C DEB passes over latitudes between 97.0°N and 97.0°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 41 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 394 km altitude. Its 97.0° 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 92 minutes, travelling at 27,635 km/h.
FENGYUN 1C DEB (NORAD ID 32203) 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: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 1C DEB (NORAD ID 32203) 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 27,635 km/h (17,171 mph) — roughly 7.68 km/s. It completes 15.58 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 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 7.68 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.