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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 OBJECT AE
1 62405U 24247AE 26093.86160011 .00101336 00000-0 15987-2 0 9995
2 62405 44.9767 301.2655 0009141 214.2223 145.8081 15.52489015 71442Epoch: 2026-04-03T20:40Z
TLE epoch observation values (Epoch: 2026-04-03T20:40:42.249Z)
Latitude
-0.00002°
Longitude
158.8998°
Altitude
414.591 km
Speed
7.661 km/s
True Right ascension
20h 05m 03s
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
19:15:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
417.298 km
Perigee altitude
404.886 km
Semi-major axis
6,789.229 km
Eccentricity
0.00091
Inclination
44.9767°
RAAN
301.2655°
Arg. of periapsis
214.2223°
True anomaly
145.86691°
Mean anomaly
145.8081°
Eccentric anomaly
145.83751°
Mean motion
3.87983 °/min
Orbital period
92.79 mins
BSTAR
0.0015987
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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 | 2026-04-04 16:57:55.848Z | 216.213° SW | 2026-04-04 16:59:55.848Z | 160.306° S | 34.824° | 2026-04-04 17:02:55.848Z | 77.722° E |
| 4 mins | 2026-04-04 18:35:55.848Z | 290.983° WNW | 2026-04-04 18:36:55.848Z | 326.575° NNW | 34.024° | 2026-04-04 18:39:55.848Z | 57.415° ENE |
| 4 mins | 2026-04-04 20:12:55.848Z | 309.513° NW | 2026-04-04 20:14:55.848Z | 9.582° NNE | 28.719° | 2026-04-04 20:16:55.848Z | 62.733° ENE |
| 4 mins | 2026-04-04 21:50:55.848Z | 300.702° NW | 2026-04-04 21:51:55.848Z | 326.251° NNW | 43.108° | 2026-04-04 21:54:55.848Z | 108.71° 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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