FENGYUN 2E
NORAD 33463
Payload
GEO
2008-066A
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GEO · NORAD 33463
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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
36113 km
Apogee
36114 km
Inclination
9.3°
Period
1452.8 min
Mean Motion
0.99117331 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,114 km
Orbital Velocity11,027 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0000
Semi-Major Axis42,485 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
2008-12-23
Launch Site
Xichang, China
Int'l Designator
2008-066A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
FENGYUN 2E is an active satellite operated by China Meteorological Administration (China), launched on 2008-12-23 from Xichang, China. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 36,113 km and 36,114 km with an inclination of 9.3°. It travels at approximately 11,027 km/h (3.06 km/s), completing one full orbit every 24.2 hours — that’s roughly 0.99 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks FENGYUN 2E 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 2E occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 9.3°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of FENGYUN 2E’s average altitude, there are currently 184 active payloads and 8 tracked debris or rocket body fragments. China operates approximately 1,219 active satellites in total, of which 14 share a similar altitude band with FENGYUN 2E.
❓ Frequently Asked Questions
FENGYUN 2E orbits at approximately 36,114 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,027 km/h — it just keeps pace with the ground below. With an inclination of 9.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
FENGYUN 2E is operated by China Meteorological Administration (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 33463. You can track FENGYUN 2E in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
FENGYUN 2E was launched on 2008-12-23 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 2E (NORAD ID 33463) 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 2E travels at approximately 11,027 km/h (6,852 mph) — roughly 3.06 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.