OBJECT AE, 62405
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
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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Edit Public Description
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: 22 hours ago
TLE from 22 hours ago
0 OBJECT AE
1 62405U 24247AE 26023.20708993 .00065624 00000-0 13952-2 0 9992
2 62405 44.9815 339.3351 0007875 92.6119 267.5672 15.44155880 60497Epoch: 2026-01-23T04:58Z
TLE epoch observation values (Epoch: 2026-01-23T04:58:12.569Z)
Latitude
-0.00002°
Longitude
142.2335°
Altitude
434.088 km
Speed
7.653 km/s
True Right ascension
22h 37m 20s
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
04:34:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
440.849 km
Perigee altitude
430.118 km
Semi-major axis
6,813.62 km
Eccentricity
0.00079
Inclination
44.9815°
RAAN
339.3351°
Arg. of periapsis
92.6119°
True anomaly
267.47704°
Mean anomaly
267.5672°
Eccentric anomaly
267.52212°
Mean motion
3.85901 °/min
Orbital period
93.29 mins
BSTAR
0.0013952
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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 | 2026-01-24 04:41:12.408Z | 300.776° NW | 2026-01-24 04:44:12.408Z | 59.051° ENE | 38.328° | 2026-01-24 04:46:12.408Z | 96.358° ESE |
| 4 mins | 2026-01-24 23:05:12.408Z | 176.475° S | 2026-01-24 23:06:12.408Z | 152.703° SSE | 20.502° | 2026-01-24 23:09:12.408Z | 90.756° ESE |
| 5 mins | 2026-01-25 00:42:12.408Z | 259.554° W | 2026-01-25 00:44:12.408Z | 13.42° NNE | 42.62° | 2026-01-25 00:47:12.408Z | 63.633° ENE |
| 4 mins | 2026-01-25 02:20:12.408Z | 304.798° NW | 2026-01-25 02:22:12.408Z | 7.58° NNE | 28.705° | 2026-01-25 02:24:12.408Z | 56.291° ENE |
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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