FENGYUN 2C
NORAD 28451
Payload
GEO
2004-042A
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GEO · NORAD 28451
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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
36396 km
Apogee
36428 km
Inclination
12.4°
Period
1468.2 min
Mean Motion
0.98081737 rev/day
TLE Epoch
2026-06-18 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,412 km
Orbital Velocity10,988 km/h
Velocity3.05 km/s
Orbital Period24.5 hours
Orbits / Day0.98
Eccentricity0.0004
Semi-Major Axis42,783 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
2004-10-19
Launch Site
Xichang, China
Int'l Designator
2004-042A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
FENGYUN 2C is an active satellite operated by China Meteorological Administration (China), launched on 2004-10-19 from Xichang, China. With over 22 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,396 km and 36,428 km with an inclination of 12.4°. It travels at approximately 10,988 km/h (3.05 km/s), completing one full orbit every 24.5 hours — that’s roughly 0.98 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 2C 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 2C 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 12.4°, 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 2C’s average altitude, there are currently 18 active payloads and 22 tracked debris or rocket body fragments. China operates approximately 1,219 active satellites in total, of which 2 share a similar altitude band with FENGYUN 2C.
❓ Frequently Asked Questions
FENGYUN 2C orbits at approximately 36,412 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 10,988 km/h — it just keeps pace with the ground below. With an inclination of 12.4°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
FENGYUN 2C is operated by China Meteorological Administration (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28451. You can track FENGYUN 2C in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
FENGYUN 2C was launched on 2004-10-19 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 2C (NORAD ID 28451) 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 2C travels at approximately 10,988 km/h (6,828 mph) — roughly 3.05 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.