NORAD 57490
FENGYUN 3F
Time
- Local time
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Position
- Latitude
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- Longitude
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- Altitude
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Speed
- Miles per hour
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- Kilometers per second
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- Miles per second
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From your location
- Azimuth
- -
- Elevation
- -
- Right ascension
- -
- Declination
- -
- Local sidereal time
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Sunlight
- Day / night
- -
Identity
- NORAD ID
- 57490
- International designator
- 2023-111A
- Launch date
- Aug 3, 2023
- Launch site
- Jiuquan Satellite Launch Center, China
- Radar size (RCS)
- Large (over 1 m²)
Radio
- Uplink
- -
- Downlink
- 2,246.403 MHz · FM2,264.641 MHz · BPSK7,790.000 MHz · AHRPT
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8,212.500 MHz · FM - Beacon
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- Mode
- AHRPT, BPSK, FM
Active transmitters from SatNOGS DB, licensed CC BY-SA 4.0.
Your station
- Grid locator
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Live
- Azimuth
- -
- Elevation
- -
- Range
- -
- Range rate
- -
- Naked-eye visibility
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- Sub-satellite grid
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- Footprint diameter
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Upcoming passes
Next 48 h · your local timeUse your location to predict passes.
Mutual visibility
With another station · next 48 hUse your location to find mutual windows.
Transmitters
Nominal · add location for DopplerMode S - TLM
Transmitter · Meteorological · FM
- Downlink
- 2,246.403 MHz
- CTCSS
- -
- Baud
- -
S-band telemetry
Transmitter · BPSK
- Downlink
- 2,264.641 MHz
- CTCSS
- -
- Baud
- 24,000
AHRPT
Transmitter · Meteorological · AHRPT
- Downlink
- 7,790.000 MHz
- CTCSS
- -
- Baud
- -
Recent receptions
SatNOGS Network-
Orbit data
- TLE epoch
- 2026-10-18 06:54:21 UTC
- TLE age
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Radio data from SatNOGS DB and SatNOGS Network, licensed CC BY-SA 4.0.
About FENGYUN 3F
FENGYUN 3F is a satellite from China, launched on Aug 3, 2023 from Jiuquan Satellite Launch Center, China.
It circles Earth every 101 minutes (14.2 times a day), between 824 and 827 km up, on an orbit tilted 98.7° to the equator, so its path covers latitudes up to 81° north and south.
The map shows where it is right now; the pass list tells you when it next comes over your location.
Orbit height over the past year
Over the last 366 days its lowest point went from 825 km to 824 km. Sudden rises are engine burns that lift the orbit; slow declines are drag from the thin upper atmosphere.
From Space-Track element sets, one point a day.