OBJECT F, 43836 (Decayed)
Orbit data source: Space-Track
OBJECT F, 43836 was a satellite in LEO that was launched on Fri, 07 Dec 2018 UTC via a CHANG ZHENG 2D launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.
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43836 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT F
1 43836U 18102F 25021.33289307 .18295486 18183-2 60627-3 0 9991
2 43836 97.3870 115.3241 0009265 285.6082 74.4198 16.46737163339248Epoch: 2025-01-21T07:59Z
TLE epoch observation values (Epoch: 2025-01-21T07:59:21.961Z)
Latitude
-0.00003°
Longitude
-125.45803°
Altitude
149.583 km
Speed
7.817 km/s
True Right ascension
07h 41m 17s
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
12:45:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
150.784 km
Perigee altitude
138.697 km
Semi-major axis
6,522.877 km
Eccentricity
0.00093
Inclination
97.387°
RAAN
115.3241°
Arg. of periapsis
285.6082°
True anomaly
74.5221°
Mean anomaly
74.4198°
Eccentric anomaly
74.47095°
Mean motion
4.11988 °/min
Orbital period
87.38 mins
BSTAR
0.00060627
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Other satellites on launch #102 in the year 2018 (2018-12-07 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.OBJECT F 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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| This satellite is decayed. |
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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