FENGYUN 2E, 33463
Orbit data source: Space-Track
FENGYUN 2E, 33463 is a payload satellite owned by CNMSC (CN) in GEO that was launched on Tue, 23 Dec 2008 UTC via a CHANG ZHENG 3A launch vehicle from the Xichang Space Center, China (XSC). 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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33463 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SISE
Mission
Non-operational Civil Weather
Bus & Motor
FY-2, SHANXI AKM
Mass
1,390 kg wet, ~600 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl, 1.5 m
Radar Cross Section
6.680 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FENGYUN 2E
1 33463U 08066A 26172.34092531 .00000035 00000-0 00000+0 0 9991
2 33463 9.2777 54.2095 0000417 355.0168 233.7324 0.99117447 64048Epoch: 2026-06-21T08:10Z
TLE epoch observation values (Epoch: 2026-06-21T08:10:55.946Z)
Latitude
-6.98563°
Longitude
-109.6775°
Altitude
36,115.126 km
Speed
3.063 km/s
True Right ascension
18h 50m 23s
True Declination
-6° 58' 43"
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
23:07:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,116.128 km
Perigee altitude
36,112.585 km
Semi-major axis
42,492.494 km
Eccentricity
0.00004
Inclination
9.2777°
RAAN
54.2095°
Arg. of periapsis
355.0168°
True anomaly
233.72855°
Mean anomaly
233.7324°
Eccentric anomaly
233.73047°
Mean motion
0.24778 °/min
Orbital period
1,452.87 mins
BSTAR
0
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Other satellites on launch #66 in the year 2008 (2008-12-23 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 2E 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-06-22 12:05:41.885Z | 191.506° SSW | 2026-06-22 23:19:41.885Z | 200.639° SSW | 38.483° | 2026-06-23 12:05:41.885Z | 196.785° SSW |
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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