Skip to content
Home Library Satellite Directory FENGYUN 2A

FENGYUN 2A

NORAD 24834 Payload GEO 1997-029A ● Active
CONNECTING… GEO · NORAD 24834
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
36562 km
Apogee
37464 km
Inclination
15.7°
Period
1499.2 min
Mean Motion
0.96050693 rev/day
TLE Epoch
2026-06-18 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,013 km
Orbital Velocity10,912 km/h
Velocity3.03 km/s
Orbital Period25.0 hours
Orbits / Day0.96
Eccentricity0.0104
Semi-Major Axis43,384 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
1997-06-10
Launch Site
Xichang, China
Int'l Designator
1997-029A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
FENGYUN 2A is an active satellite operated by China Meteorological Administration (China), launched on 1997-06-10 from Xichang, China. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,562 km and 37,464 km with an inclination of 15.7°. It travels at approximately 10,912 km/h (3.03 km/s), completing one full orbit every 25.0 hours — that’s roughly 0.96 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 2A 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 2A 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 15.7°, 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 2A’s average altitude, there are currently 6 active payloads and 2 tracked debris or rocket body fragments. China operates approximately 1,218 active satellites in total.
❓ Frequently Asked Questions
FENGYUN 2A orbits at approximately 37,013 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 10,912 km/h — it just keeps pace with the ground below. With an inclination of 15.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
FENGYUN 2A is operated by China Meteorological Administration (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24834. You can track FENGYUN 2A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
FENGYUN 2A was launched on 1997-06-10 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 2A (NORAD ID 24834) 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 2A travels at approximately 10,912 km/h (6,780 mph) — roughly 3.03 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.