FENGYUN 1B
NORAD 20788
Payload
LEO
1990-081A
● Active
CONNECTING…
LEO · NORAD 20788
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
872 km
Apogee
894 km
Inclination
99.0°
Period
102.6 min
Mean Motion
14.03200891 rev/day
TLE Epoch
2026-06-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude883 km
Orbital Velocity26,686 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.03
Eccentricity0.0015
Semi-Major Axis7,254 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Meteorological Administration (China)
Launch Date
1990-09-03
Launch Site
Taiyuan, China
Int'l Designator
1990-081A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
FENGYUN 1B is an active satellite operated by China Meteorological Administration (China), launched on 1990-09-03 from Taiyuan, China. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 872 km and 894 km with an inclination of 99.0°. It travels at approximately 26,686 km/h (7.41 km/s), completing one full orbit every 103 minutes — that’s roughly 14.03 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks FENGYUN 1B 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 1B orbits at an average altitude of 883 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 1B’s average altitude, there are currently 210 active payloads and 1,591 tracked debris or rocket body fragments. With an inclination of 99.0°, FENGYUN 1B passes over latitudes between 99.0°N and 99.0°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 1,219 active satellites in total, of which 119 share a similar altitude band with FENGYUN 1B.
❓ Frequently Asked Questions
FENGYUN 1B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 883 km altitude. Its 99.0° 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 103 minutes, travelling at 26,686 km/h.
FENGYUN 1B is operated by China Meteorological Administration (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 20788. You can track FENGYUN 1B in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
FENGYUN 1B was launched on 1990-09-03 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks FENGYUN 1B (NORAD ID 20788) 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 1B travels at approximately 26,686 km/h (16,582 mph) — roughly 7.41 km/s. It completes 14.03 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.