OBJECT X, 62398 (Decayed)
Orbit data source: Space-Track
OBJECT X, 62398 was a satellite in LEO that was launched on Sat, 21 Dec 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62398 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 OBJECT X
1 62398U 24247X 26073.16816966 .13173731 10423-4 12170-2 0 9991
2 62398 44.9756 24.6545 0005579 218.4439 141.6088 16.37774077 69224Epoch: 2026-03-14T04:02Z
TLE epoch observation values (Epoch: 2026-03-14T04:02:09.858Z)
Latitude
-0.00008°
Longitude
152.32013°
Altitude
174.591 km
Speed
7.802 km/s
True Right ascension
01h 38m 37s
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
22:16:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
177.075 km
Perigee altitude
169.765 km
Semi-major axis
6,551.557 km
Eccentricity
0.00056
Inclination
44.9756°
RAAN
24.6545°
Arg. of periapsis
218.4439°
True anomaly
141.64848°
Mean anomaly
141.6088°
Eccentric anomaly
141.62864°
Mean motion
4.09286 °/min
Orbital period
87.96 mins
BSTAR
0.001217
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Other satellites on launch #247 in the year 2024 (2024-12-21 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 X 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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