FENGYUN 3E
NORAD 49008
Payload
LEO
2021-062A
● Active
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LEO · NORAD 49008
NOW PASSING OVER
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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
824 km
Apogee
828 km
Inclination
98.8°
Period
101.4 min
Mean Motion
14.19902876 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude826 km
Orbital Velocity26,791 km/h
Velocity7.44 km/s
Orbital Period101 minutes
Orbits / Day14.20
Eccentricity0.0003
Semi-Major Axis7,197 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
2021-07-04
Launch Site
Jiuquan, China
Int'l Designator
2021-062A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
FENGYUN 3E is an active satellite operated by China Meteorological Administration (China), launched on 2021-07-04 from Jiuquan, China. It orbits in Low Earth Orbit (LEO) at altitudes between 824 km and 828 km with an inclination of 98.8°. It travels at approximately 26,791 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks FENGYUN 3E 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 3E orbits at an average altitude of 826 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 3E’s average altitude, there are currently 370 active payloads and 2,257 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.8°, FENGYUN 3E passes over latitudes between 98.8°N and 98.8°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 111 share a similar altitude band with FENGYUN 3E.
❓ Frequently Asked Questions
FENGYUN 3E is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 826 km altitude. Its 98.8° 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 26,791 km/h.
FENGYUN 3E is operated by China Meteorological Administration (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 49008. You can track FENGYUN 3E in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
FENGYUN 3E was launched on 2021-07-04 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 3E (NORAD ID 49008) 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 3E travels at approximately 26,791 km/h (16,647 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.