FENGYUN 2B
NORAD 26382
Payload
GEO
2000-032A
● Active
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GEO · NORAD 26382
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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
35822 km
Apogee
35847 km
Inclination
13.3°
Period
1438.5 min
Mean Motion
1.00101341 rev/day
TLE Epoch
2026-06-18 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,835 km
Orbital Velocity11,063 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0003
Semi-Major Axis42,206 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
2000-06-25
Launch Site
Xichang, China
Int'l Designator
2000-032A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
FENGYUN 2B is an active satellite operated by China Meteorological Administration (China), launched on 2000-06-25 from Xichang, China. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,822 km and 35,847 km with an inclination of 13.3°. It travels at approximately 11,063 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 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 2B 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 2B 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 13.3°, 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 2B’s average altitude, there are currently 668 active payloads and 55 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. China operates approximately 1,219 active satellites in total, of which 106 share a similar altitude band with FENGYUN 2B.
❓ Frequently Asked Questions
FENGYUN 2B orbits at approximately 35,835 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 11,063 km/h — it just keeps pace with the ground below. With an inclination of 13.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
FENGYUN 2B is operated by China Meteorological Administration (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26382. You can track FENGYUN 2B in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
FENGYUN 2B was launched on 2000-06-25 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 2B (NORAD ID 26382) 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 2B travels at approximately 11,063 km/h (6,874 mph) — roughly 3.07 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.