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FENGYUN 3A

NORAD 32958 Payload LEO 2008-026A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
820 km
Apogee
834 km
Inclination
98.7°
Period
101.4 min
Mean Motion
14.19548950 rev/day
TLE Epoch
2026-03-17 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude827 km
Orbital Velocity26,790 km/h
Velocity7.44 km/s
Orbital Period101 minutes
Orbits / Day14.20
Eccentricity0.0010
Semi-Major Axis7,198 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2008-05-27
Launch Site
Taiyuan, China
Int'l Designator
2008-026A
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
weather
📖 About This Object
FENGYUN 3A is an active satellite operated by China, launched on 2008-05-27 from Taiyuan, China. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 820 km and 834 km with an inclination of 98.7°. It travels at approximately 26,790 km/h (7.44 km/s), completing one full orbit every 101 minutes — that’s roughly 14.20 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. It is part of the Weather constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks FENGYUN 3A 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 3A operates in a sun-synchronous orbit (SSO), a special subset of LEO where the orbital plane precesses to keep a constant angle relative to the Sun. This means the satellite crosses any given latitude at approximately the same local solar time on every pass, providing consistent lighting conditions — essential for Earth observation, weather monitoring and environmental science. SSO orbits typically sit between 600 and 800 km altitude with inclinations near 97–99°.
❓ Frequently Asked Questions
FENGYUN 3A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 827 km altitude. Its 98.7° 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 101 minutes, travelling at 26,790 km/h.
FENGYUN 3A is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 32958. You can track FENGYUN 3A in real time on Orbital Radar’s live tracker.
FENGYUN 3A was launched on 2008-05-27 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years.
Yes — Orbital Radar tracks FENGYUN 3A (NORAD ID 32958) 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.
FENGYUN 3A travels at approximately 26,790 km/h (16,646 mph) — roughly 7.44 km/s. It completes 14.20 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.
FENGYUN 3A is a member of the Weather constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Weather satellites on Orbital Radar’s live tracker.