OBJECT S, 62393
Orbit data source: Space-Track
OBJECT S, 62393 is 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.
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62393 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 OBJECT S
1 62393U 24247S 26168.43352350 .08555031 10449-4 12024-2 0 9990
2 62393 44.9438 214.8221 0004217 356.8938 3.1957 16.33986744 83897Epoch: 2026-06-17T10:24Z
TLE epoch observation values (Epoch: 2026-06-17T10:24:16.430Z)
Latitude
-0.00007°
Longitude
153.0623°
Altitude
179.078 km
Speed
7.802 km/s
True Right ascension
14h 19m 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
07:19:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
186.307 km
Perigee altitude
180.773 km
Semi-major axis
6,561.677 km
Eccentricity
0.00042
Inclination
44.9438°
RAAN
214.8221°
Arg. of periapsis
356.8938°
True anomaly
3.1984°
Mean anomaly
3.1957°
Eccentric anomaly
3.19705°
Mean motion
4.08339 °/min
Orbital period
88.16 mins
BSTAR
0.0012024
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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 S 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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| OBJECT S is likely not visible in the next few days. |
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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