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FENGYUN 3B

Fengyun-3B, launched in 2010, continued China's second-generation polar meteorological program and expanded global environmental observations.

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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°

These are representative calculations derived from current orbital elements, not fixed physical specifications. Altitude and speed change around an elliptical orbit, and predictions change as new orbital elements are published.

Launch record

Launch and deployment

Fengyun-3B launched on 4 November 2010 aboard a Long March 4C from Taiyuan.

TransitSatellite does not estimate historical launch weather. Temperature, clouds, wind, holds, and scrub reasons will appear only when supported by traceable historical sources.

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

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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