FENGYUN 2H DEB, 43645
Orbit data source: Space-Track
FENGYUN 2H DEB, 43645 is space debris in GEO originally from a launch on Tue, 05 Jun 2018 UTC launched from the Xichang Space Center, China (XSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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43645 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FENGYUN 2H DEB
1 43645U 18050D 25260.05915169 .00000021 00000-0 00000-0 0 9990
2 43645 4.1947 79.7249 0039091 251.1207 108.7582 1.00229224 26187
Epoch: 2025-09-17T01:25Z
TLE epoch observation values (Epoch: 2025-09-17T01:25:10.706Z)
Latitude
0°
Longitude
62.48837°
Altitude
35,851.383 km
Speed
3.07 km/s
True Right ascension
05h 20m 05s
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
12:48:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,964.469 km
Perigee altitude
35,634.715 km
Semi-major axis
42,177.729 km
Eccentricity
0.00391
Inclination
4.1947°
RAAN
79.7249°
Arg. of periapsis
251.1207°
True anomaly
109.18169°
Mean anomaly
108.7582°
Eccentric anomaly
108.97001°
Mean motion
0.25056 °/min
Orbital period
1,436.76 mins
BSTAR
0
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Other satellites on launch #50 in the year 2018 (2018-06-05 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 2H DEB Visibility
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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. |
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FENGYUN 2H DEB is likely not visible in the next few days. |
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43645 neighbors
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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
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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