FENGYUN 1C DEB
NORAD 29954
Debris
LEO
1999-025KC
CONNECTING…
LEO · NORAD 29954
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
721 km
Apogee
828 km
Inclination
100.1°
Period
100.3 min
Mean Motion
14.35108873 rev/day
TLE Epoch
2026-06-26 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude775 km
Orbital Velocity26,888 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.35
Eccentricity0.0075
Semi-Major Axis7,146 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
1999-05-10
Launch Site
Taiyuan, China
Int'l Designator
1999-025KC
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 721 km and 828 km with an inclination of 100.1°. It travels at approximately 26,888 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.35 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 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 775 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of FENGYUN 1C DEB’s average altitude, there are currently 404 active payloads and 2,143 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179, ONEWEB-0455. With an inclination of 100.1°, FENGYUN 1C DEB passes over latitudes between 100.1°N and 100.1°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, of which 77 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 721 km (perigee) and 828 km (apogee), with an average altitude of approximately 775 km. It completes one orbit every 100 minutes, travelling at approximately 26,888 km/h (16,707 mph).
FENGYUN 1C DEB (NORAD ID 29954) 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 1C DEB (NORAD ID 29954) 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 26,888 km/h (16,707 mph) — roughly 7.47 km/s. It completes 14.35 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 7.47 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.