OBJECT P, 62390 (Decayed)
Orbit data source: Space-Track
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Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT P, 62390 was a satellite in LEO that was launched on Sat, 21 Dec 2024 UTC launched 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. This object's orbit decayed before it could be identified.
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62390 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 OBJECT P
1 62390U 24247P 25005.72872000 .00016217 00000-0 81076-3 0 9999
2 62390 44.9991 278.8774 0001451 324.2414 35.8368 15.17317663 2456Epoch: 2025-01-05T17:29Z
TLE epoch observation values (Epoch: 2025-01-05T17:29:21.408Z)
Latitude
0.00002°
Longitude
-89.0222°
Altitude
513.139 km
Speed
7.609 km/s
True Right ascension
18h 35m 30s
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
06:10:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.554 km
Perigee altitude
514.553 km
Semi-major axis
6,893.69 km
Eccentricity
0.00015
Inclination
44.9991°
RAAN
278.8774°
Arg. of periapsis
324.2414°
True anomaly
35.84654°
Mean anomaly
35.8368°
Eccentric anomaly
35.84167°
Mean motion
3.79198 °/min
Orbital period
94.94 mins
BSTAR
0.00081076
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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 P 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 | 2025-10-25 16:00:09.557Z | 198.834° SSW | 2025-10-25 16:03:09.557Z | 135.032° SSE | 24.332° | 2025-10-25 16:05:09.557Z | 93.57° ESE |
| 5 mins | 2025-10-25 17:39:09.557Z | 261.485° W | 2025-10-25 17:41:09.557Z | 314.467° NW | 42.105° | 2025-10-25 17:44:09.557Z | 61.198° ENE |
| 5 mins | 2025-10-25 19:18:09.557Z | 299.406° NW | 2025-10-25 19:20:09.557Z | 346.464° N | 30.247° | 2025-10-25 19:23:09.557Z | 61.645° ENE |
| 6 mins | 2025-10-25 20:57:09.557Z | 303.077° NW | 2025-10-25 20:59:09.557Z | 346.567° N | 38.28° | 2025-10-25 21:03:09.557Z | 96.427° ESE |
| 5 mins | 2025-10-25 22:36:09.557Z | 268.48° W | 2025-10-25 22:38:09.557Z | 215.737° SW | 30.108° | 2025-10-25 22:41:09.557Z | 149.782° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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