FENGYUN 3B
Fengyun-3B, launched in 2010, continued China's second-generation polar meteorological program and expanded global environmental observations.
Object identity
- NORAD ID
- 37214
- COSPAR ID
- 2010-059A
- Operator
- Not listed
- Country
- Not listed
- Launch date
- Not listed
Immediate discovery
Why this satellite matters
Constellation timing matters because multiple polar spacecraft can sample different local times of day, improving the temporal picture of changing weather systems.
Understanding the mission
Science and engineering ideas
Constellation timing matters because multiple polar spacecraft can sample different local times of day, improving the temporal picture of changing weather systems.
Mission
Mission and purpose
Weather spacecraft carry instruments that observe Earth and its atmosphere in visible, infrared, microwave, or other wavelengths. Different orbits provide either repeated regional views or broad global coverage.
- Constellation timing matters because multiple polar spacecraft can sample different local times of day, improving the temporal picture of changing weather systems.
Design
Engineering
Constellation timing matters because multiple polar spacecraft can sample different local times of day, improving the temporal picture of changing weather systems.
Real orbital values
The mathematics
The current two-line element set reports approximately 14.1486 revolutions per day. Dividing 1,440 minutes by that value gives an estimated orbital period of 101.8 minutes.
Period
101.8 min
Representative speed
26,747 km/h
Representative altitude
850 km
Inclination
98.95°
Launch record
Launch and deployment
Fengyun-3B launched on 4 November 2010 aboard a Long March 4C from Taiyuan.
Orbit
LEO orbit explained
Low Earth orbit is the region closest to Earth used by most crewed spacecraft, many science missions, Earth-observation satellites, and large constellations. Objects move quickly and commonly complete an orbit in roughly 90 to 130 minutes.
LEO can provide detailed Earth views, lower communications delay, and easier access than higher orbits, but it covers less area per spacecraft and is more affected by atmospheric drag.
Live TransitSatellite experience
See FENGYUN 3B moving now
Open the live tracker to view its current calculated position, trajectory, orbital information, visibility tools, and Save and Share controls.
Learning
Questions to explore
- Why can infrared instruments observe clouds at night?
- What is the difference between continuous regional coverage and global coverage?
Evidence
Sources and data notes
Current identity and orbital elements come from CelesTrak’s public GP data. Calculated orbit values are derived from the current TLE and may change after catalog updates. Mission-history claims are added separately and require authoritative sources.
Catalog updated
Sep 20, 2026, 1:26 PM UTC
Story review
1970-01-01T00:00:00.000Z
