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 spacecraft
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
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 OBJECT AE
1 62405U 24247AE 25238.84428301 .00025116 00000-0 80887-3 0 9995
2 62405 44.9838 87.4709 0008213 219.3482 140.6806 15.31793217 37502Epoch: 2025-08-26T20:15Z
TLE epoch observation values (Epoch: 2025-08-26T20:15:46.052Z)
Latitude
-0.00002°
Longitude
168.19883°
Altitude
474.812 km
Speed
7.628 km/s
True Right ascension
05h 49m 53s
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
16:59:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.703 km
Perigee altitude
466.451 km
Semi-major axis
6,850.214 km
Eccentricity
0.00082
Inclination
44.9838°
RAAN
87.4709°
Arg. of periapsis
219.3482°
True anomaly
140.74019°
Mean anomaly
140.6806°
Eccentric anomaly
140.7104°
Mean motion
3.82813 °/min
Orbital period
94.04 mins
BSTAR
0.00080887
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Other satellites on launch #247 in the year 2024 (2024-12-21 UTC)
OBJECT AE Visibility forecast
Observer location: undefined°, undefined°
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 | 2025-08-30 15:13:25.868Z | 188.648° SSW | 2025-08-30 15:15:25.868Z | 146.309° SSE | 22.459° | 2025-08-30 15:18:25.868Z | 88.878° E |
| 6 mins | 2025-08-30 16:51:25.868Z | 257.057° W | 2025-08-30 16:53:25.868Z | 292.109° WNW | 42.042° | 2025-08-30 16:57:25.868Z | 64.224° ENE |
| 5 mins | 2025-08-30 18:30:25.868Z | 298.956° NW | 2025-08-30 18:32:25.868Z | 348.72° N | 30.491° | 2025-08-30 18:35:25.868Z | 61.521° ENE |
| 5 mins | 2025-08-30 20:09:25.868Z | 306.241° NW | 2025-08-30 20:11:25.868Z | 6.981° NNE | 38.366° | 2025-08-30 20:14:25.868Z | 90.774° ESE |
| 5 mins | 2025-08-30 21:48:25.868Z | 263.924° W | 2025-08-30 21:50:25.868Z | 194.026° SSW | 31.353° | 2025-08-30 21:53:25.868Z | 142.916° SSE |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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