FENGYUN 1C DEB
NORAD 30863
Debris
MEO
1999-025AWZ
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MEO · NORAD 30863
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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
814 km
Apogee
2189 km
Inclination
99.1°
Period
116.0 min
Mean Motion
12.41176671 rev/day
TLE Epoch
2026-06-24 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,502 km
Orbital Velocity25,616 km/h
Velocity7.12 km/s
Orbital Period116 minutes
Orbits / Day12.41
Eccentricity0.0873
Semi-Major Axis7,873 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
1999-05-10
Launch Site
Taiyuan, China
Int'l Designator
1999-025AWZ
Object Type
Debris
RCS Size
Medium (0.1–1 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 Medium Earth Orbit (MEO) at altitudes between 814 km and 2,189 km with an inclination of 99.1°. It travels at approximately 25,616 km/h (7.12 km/s), completing one full orbit every 116 minutes — that’s roughly 12.41 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of 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 1,502 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of FENGYUN 1C DEB’s average altitude, there are currently 235 active payloads and 251 tracked debris or rocket body fragments. With an inclination of 99.1°, FENGYUN 1C DEB passes over latitudes between 99.1°N and 99.1°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 1,221 active satellites in total.
🔗 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 orbits in Medium Earth Orbit (MEO) at altitudes between 814 km (perigee) and 2,189 km (apogee), with an average altitude of approximately 1,502 km. It completes one orbit every 116 minutes, travelling at approximately 25,616 km/h (15,917 mph).
FENGYUN 1C DEB (NORAD ID 30863) 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 1C DEB (NORAD ID 30863) 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 25,616 km/h (15,917 mph) — roughly 7.12 km/s. It completes 12.41 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.12 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.