OBJECT W, 62397 (Decayed)
Orbit data source: Space-Track
OBJECT W, 62397 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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62397 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.0 m
Radar Cross Section
0.004 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 OBJECT W
1 62397U 24247W 26090.99920375 .11050862 10453-4 13120-2 0 9996
2 62397 44.9687 286.1248 0011081 277.7804 82.1861 16.35355054 71960Epoch: 2026-03-31T23:58Z
TLE epoch observation values (Epoch: 2026-03-31T23:58:51.204Z)
Latitude
-0.00007°
Longitude
97.04305°
Altitude
177.203 km
Speed
7.802 km/s
True Right ascension
19h 04m 29s
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
10:18:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
187.144 km
Perigee altitude
172.61 km
Semi-major axis
6,558.014 km
Eccentricity
0.00111
Inclination
44.9687°
RAAN
286.1248°
Arg. of periapsis
277.7804°
True anomaly
82.31192°
Mean anomaly
82.1861°
Eccentric anomaly
82.24901°
Mean motion
4.08681 °/min
Orbital period
88.09 mins
BSTAR
0.001312
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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 W 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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