FENGYUN 1A
NORAD 19467
Payload
LEO
1988-080A
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LEO · NORAD 19467
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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
872 km
Apogee
891 km
Inclination
99.0°
Period
102.6 min
Mean Motion
14.03542004 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude882 km
Orbital Velocity26,689 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.04
Eccentricity0.0013
Semi-Major Axis7,253 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
1988-09-06
Launch Site
Taiyuan, China
Int'l Designator
1988-080A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
FENGYUN 1A is an active satellite operated by China Meteorological Administration (China), launched on 1988-09-06 from Taiyuan, China. With over 38 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 872 km and 891 km with an inclination of 99.0°. It travels at approximately 26,689 km/h (7.41 km/s), completing one full orbit every 103 minutes — that’s roughly 14.04 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 1A 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 1A orbits at an average altitude of 882 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 1A’s average altitude, there are currently 194 active payloads and 1,620 tracked debris or rocket body fragments. With an inclination of 99.0°, FENGYUN 1A 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 102 share a similar altitude band with FENGYUN 1A.
❓ Frequently Asked Questions
FENGYUN 1A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 882 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 103 minutes, travelling at 26,689 km/h.
FENGYUN 1A is operated by China Meteorological Administration (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 19467. You can track FENGYUN 1A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
FENGYUN 1A was launched on 1988-09-06 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 1A (NORAD ID 19467) 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 1A travels at approximately 26,689 km/h (16,584 mph) — roughly 7.41 km/s. It completes 14.04 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.