FENGYUN 1C DEB
NORAD 30705
Debris
LEO
1999-025ARP
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LEO · NORAD 30705
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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
810 km
Apogee
1102 km
Inclination
102.2°
Period
104.2 min
Mean Motion
13.82346591 rev/day
TLE Epoch
2026-06-26 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude956 km
Orbital Velocity26,553 km/h
Velocity7.38 km/s
Orbital Period104 minutes
Orbits / Day13.82
Eccentricity0.0199
Semi-Major Axis7,327 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
1999-05-10
Launch Site
Taiyuan, China
Int'l Designator
1999-025ARP
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 Low Earth Orbit (LEO) at altitudes between 810 km and 1,102 km with an inclination of 102.2°. It travels at approximately 26,553 km/h (7.38 km/s), completing one full orbit every 104 minutes — that’s roughly 13.82 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 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 956 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of FENGYUN 1C DEB’s average altitude, there are currently 325 active payloads and 1,087 tracked debris or rocket body fragments. With an inclination of 102.2°, FENGYUN 1C DEB passes over latitudes between 102.2°N and 102.2°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 58 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 orbits in Low Earth Orbit (LEO) at altitudes between 810 km (perigee) and 1,102 km (apogee), with an average altitude of approximately 956 km. It completes one orbit every 104 minutes, travelling at approximately 26,553 km/h (16,499 mph).
FENGYUN 1C DEB (NORAD ID 30705) 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 1C DEB (NORAD ID 30705) 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 26,553 km/h (16,499 mph) — roughly 7.38 km/s. It completes 13.82 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.38 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.