OBJECT AE, 62405
Orbit data source: Space-Track
OBJECT AE, 62405 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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62405 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.004 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 OBJECT AE
1 62405U 24247AE 26171.42356804 .00070835 00000-0 77578-3 0 9995
2 62405 44.9728 218.3510 0010154 4.0201 356.0775 15.62367815 83537Epoch: 2026-06-20T10:09Z
TLE epoch observation values (Epoch: 2026-06-20T10:09:56.278Z)
Latitude
-0.00002°
Longitude
157.22809°
Altitude
373.969 km
Speed
7.691 km/s
True Right ascension
14h 33m 24s
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
08:42:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
389.322 km
Perigee altitude
375.593 km
Semi-major axis
6,760.595 km
Eccentricity
0.00102
Inclination
44.9728°
RAAN
218.351°
Arg. of periapsis
4.0201°
True anomaly
356.06953°
Mean anomaly
356.0775°
Eccentric anomaly
356.07352°
Mean motion
3.9045 °/min
Orbital period
92.2 mins
BSTAR
0.00077578
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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 AE Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 06:19:25.849Z | 215.189° SW | 2026-06-21 06:21:25.849Z | 156.648° SSE | 33.172° | 2026-06-21 06:24:25.849Z | 77.541° E |
| 4 mins | 2026-06-21 07:56:25.849Z | 284.841° WNW | 2026-06-21 07:58:25.849Z | 8.806° NNE | 32.669° | 2026-06-21 08:00:25.849Z | 55.54° ENE |
| 4 mins | 2026-06-21 09:33:25.849Z | 315.282° NNW | 2026-06-21 09:35:25.849Z | 24.361° NE | 26.03° | 2026-06-21 09:37:25.849Z | 66.521° ENE |
| 4 mins | 2026-06-21 11:10:25.849Z | 302.47° NW | 2026-06-21 11:11:25.849Z | 333.028° NNW | 42.53° | 2026-06-21 11:14:25.849Z | 107.17° ESE |
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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