OBJECT J, 62385
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 J, 62385 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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62385 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, 0.0 m
Radar Cross Section
0.004 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 OBJECT J
1 62385U 24247J 25349.29265605 .00018238 00000-0 49530-3 0 9997
2 62385 45.0001 201.4807 0009718 209.6475 150.3862 15.37338414 55022Epoch: 2025-12-15T07:01Z
TLE epoch observation values (Epoch: 2025-12-15T07:01:25.482Z)
Latitude
-0.00002°
Longitude
11.9312°
Altitude
459.755 km
Speed
7.635 km/s
True Right ascension
13h 25m 55s
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
23:41:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.241 km
Perigee altitude
448.959 km
Semi-major axis
6,833.737 km
Eccentricity
0.00097
Inclination
45.0001°
RAAN
201.4807°
Arg. of periapsis
209.6475°
True anomaly
150.44117°
Mean anomaly
150.3862°
Eccentric anomaly
150.41369°
Mean motion
3.84199 °/min
Orbital period
93.7 mins
BSTAR
0.0004953
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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 J 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 | 2025-12-16 17:34:01.967Z | 226.438° WSW | 2025-12-16 17:36:01.967Z | 126.897° SE | 41.533° | 2025-12-16 17:39:01.967Z | 71.235° E |
| 5 mins | 2025-12-16 19:12:01.967Z | 288.568° WNW | 2025-12-16 19:14:01.967Z | 347.576° N | 33.317° | 2025-12-16 19:17:01.967Z | 59.044° ENE |
| 4 mins | 2025-12-16 20:51:01.967Z | 315.328° NNW | 2025-12-16 20:53:01.967Z | 24.808° NE | 31.192° | 2025-12-16 20:55:01.967Z | 71.042° E |
| 5 mins | 2025-12-16 22:29:01.967Z | 289.068° WNW | 2025-12-16 22:31:01.967Z | 195.898° SSW | 44.323° | 2025-12-16 22:34:01.967Z | 120.511° SE |
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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