FENGYUN 3E, 49008
Orbit data source: Space-Track
FENGYUN 3E, 49008 is a payload satellite owned by CNMSC (CN) in SSO that was launched on Sun, 04 Jul 2021 UTC via a CHANG ZHENG 4C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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49008 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SISE
Mission
Operational Civil Weather
Bus & Motor
FY-3, Unknown motor
Mass
2,450 kg wet, 2,250 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 5.0 m
Radar Cross Section
15.104 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 FENGYUN 3E
1 49008U 21062A 26172.50017913 .00000183 00000-0 10675-3 0 9990
2 49008 98.7495 175.8605 0002823 78.9678 281.1816 14.19904829257195Epoch: 2026-06-21T12:00Z
TLE epoch observation values (Epoch: 2026-06-21T12:00:15.476Z)
Latitude
-0.00002°
Longitude
86.09646°
Altitude
828.194 km
Speed
7.439 km/s
True Right ascension
11h 43m 26s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:38:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
824.868 km
Perigee altitude
820.802 km
Semi-major axis
7,200.972 km
Eccentricity
0.00028
Inclination
98.7495°
RAAN
175.8605°
Arg. of periapsis
78.9678°
True anomaly
281.14986°
Mean anomaly
281.1816°
Eccentric anomaly
281.16573°
Mean motion
3.55187 °/min
Orbital period
101.36 mins
BSTAR
0.00010675
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Other satellites on launch #62 in the year 2021 (2021-07-04 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.FENGYUN 3E Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-22 12:16:23.679Z | 38.522° NE | 2026-06-22 12:20:23.679Z | 90.529° ESE | 25.707° | 2026-06-22 12:24:23.679Z | 149.484° SSE |
| 8 mins | 2026-06-22 13:57:23.679Z | 347.379° N | 2026-06-22 14:00:23.679Z | 302.576° NW | 29.383° | 2026-06-22 14:05:23.679Z | 229.34° WSW |
| 8 mins | 2026-06-22 23:39:23.679Z | 135.626° SSE | 2026-06-22 23:43:23.679Z | 59.268° ENE | 35.408° | 2026-06-22 23:47:23.679Z | 1.79° NNE |
| 6 mins | 2026-06-23 01:21:23.679Z | 236.191° WSW | 2026-06-23 01:23:23.679Z | 265.507° W | 20.301° | 2026-06-23 01:27:23.679Z | 315.084° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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