OBJECT AE, 63238
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, 63238 is a satellite in SSO that was launched on Sat, 15 Mar 2025 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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63238 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Defense Calibration
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 OBJECT AE
1 63238U 25052AE 25347.20866746 .00025519 00000-0 10217-2 0 9991
2 63238 97.4144 238.5009 0009406 81.0079 279.2223 15.25002114 41614Epoch: 2025-12-13T05:00Z
TLE epoch observation values (Epoch: 2025-12-13T05:00:28.868Z)
Latitude
-0.00003°
Longitude
81.24139°
Altitude
492.846 km
Speed
7.619 km/s
True Right ascension
15h 54m 00s
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
18:32:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.197 km
Perigee altitude
481.281 km
Semi-major axis
6,865.876 km
Eccentricity
0.00094
Inclination
97.4144°
RAAN
238.5009°
Arg. of periapsis
81.0079°
True anomaly
279.11589°
Mean anomaly
279.2223°
Eccentric anomaly
279.1691°
Mean motion
3.81504 °/min
Orbital period
94.36 mins
BSTAR
0.0010217
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Other satellites on launch #52 in the year 2025 (2025-03-15 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 | 2025-12-14 05:11:43.843Z | 37.705° NE | 2025-12-14 05:14:43.843Z | 99.723° ESE | 25.12° | 2025-12-14 05:17:43.843Z | 157.43° SSE |
| 5 mins | 2025-12-14 17:21:43.843Z | 197.745° SSW | 2025-12-14 17:23:43.843Z | 250.41° W | 33.397° | 2025-12-14 17:26:43.843Z | 329.672° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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