Skip to content
Home Library Satellite Directory FENGYUN 1D

FENGYUN 1D

NORAD 27431 Payload LEO 2002-024B ● Active
CONNECTING… LEO · NORAD 27431
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
848 km
Apogee
869 km
Inclination
99.0°
Period
102.1 min
Mean Motion
14.10224851 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude859 km
Orbital Velocity26,731 km/h
Velocity7.43 km/s
Orbital Period102 minutes
Orbits / Day14.10
Eccentricity0.0015
Semi-Major Axis7,230 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
2002-05-15
Launch Site
Taiyuan, China
Int'l Designator
2002-024B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
FENGYUN 1D is an active satellite operated by China Meteorological Administration (China), launched on 2002-05-15 from Taiyuan, China. With over 24 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 848 km and 869 km with an inclination of 99.0°. It travels at approximately 26,731 km/h (7.43 km/s), completing one full orbit every 102 minutes — that’s roughly 14.10 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 ~100–500 years. Orbital Radar tracks FENGYUN 1D in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
FENGYUN 1D orbits at an average altitude of 859 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 1D’s average altitude, there are currently 255 active payloads and 1,937 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 99.0°, FENGYUN 1D 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 1,218 active satellites in total, of which 129 share a similar altitude band with FENGYUN 1D.
❓ Frequently Asked Questions
FENGYUN 1D is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 859 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 102 minutes, travelling at 26,731 km/h.
FENGYUN 1D is operated by China Meteorological Administration (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27431. You can track FENGYUN 1D in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
FENGYUN 1D was launched on 2002-05-15 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 1D (NORAD ID 27431) 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 1D travels at approximately 26,731 km/h (16,610 mph) — roughly 7.43 km/s. It completes 14.10 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.