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
ONDO Space LLC (US)Manufacturer
ONDO Space
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 0.5U, Unknown motor
Mass
0.25 kg wet, 0.25 kg dry
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: 1 day ago
TLE from 1 day ago
0 OBJECT AE
1 62405U 24247AE 25348.30846030 .00037819 00000-0 91098-3 0 9990
2 62405 44.9796 202.1354 0009840 199.4222 160.6292 15.40635816 54335Epoch: 2025-12-14T07:24Z
TLE epoch observation values (Epoch: 2025-12-14T07:24:10.969Z)
Latitude
-0.00003°
Longitude
7.86642°
Altitude
450.561 km
Speed
7.64 km/s
True Right ascension
13h 28m 32s
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
17:08:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
452.568 km
Perigee altitude
439.139 km
Semi-major axis
6,823.99 km
Eccentricity
0.00098
Inclination
44.9796°
RAAN
202.1354°
Arg. of periapsis
199.4222°
True anomaly
160.66656°
Mean anomaly
160.6292°
Eccentric anomaly
160.64788°
Mean motion
3.85022 °/min
Orbital period
93.5 mins
BSTAR
0.00091098
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-15 19:29:35.073Z | 282.551° WNW | 2025-12-15 19:32:35.073Z | 344.839° N | 31.527° | 2025-12-15 19:35:35.073Z | 58.988° ENE |
| 4 mins | 2025-12-15 21:09:35.073Z | 317.168° NNW | 2025-12-15 21:11:35.073Z | 33.593° NE | 31.589° | 2025-12-15 21:13:35.073Z | 76.377° E |
| 4 mins | 2025-12-15 22:47:35.073Z | 280.024° WNW | 2025-12-15 22:49:35.073Z | 165.664° S | 39.742° | 2025-12-15 22:51:35.073Z | 129.443° SE |
| 5 mins | 2025-12-16 17:12:35.073Z | 224.425° SW | 2025-12-16 17:14:35.073Z | 129.662° SE | 40.774° | 2025-12-16 17:17:35.073Z | 71.882° E |
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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