OBJECT AE, 63238
Orbit data source: Space-Track
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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Identifier
Orbit
Country
TBDRelated business
Tel Aviv University (IL)Manufacturer
ISA/TAU
Mission
Operational Defense Calibration
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
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: 13 hours ago
TLE from 13 hours ago
0 OBJECT AE
1 63238U 25052AE 26129.70074179 .00010919 00000-0 37295-3 0 9990
2 63238 97.3979 25.0611 0004165 282.2953 77.7822 15.30471471 64130Epoch: 2026-05-09T16:49Z
TLE epoch observation values (Epoch: 2026-05-09T16:49:04.090Z)
Latitude
0.00003°
Longitude
-94.72035°
Altitude
476.906 km
Speed
7.628 km/s
True Right ascension
01h 40m 14s
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
13:33:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.209 km
Perigee altitude
468.503 km
Semi-major axis
6,849.493 km
Eccentricity
0.00042
Inclination
97.3979°
RAAN
25.0611°
Arg. of periapsis
282.2953°
True anomaly
77.82885°
Mean anomaly
77.7822°
Eccentric anomaly
77.80553°
Mean motion
3.82874 °/min
Orbital period
94.03 mins
BSTAR
0.00037295
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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 | 2026-05-10 05:55:44.709Z | 9.521° NNE | 2026-05-10 05:58:44.709Z | 282.1° WNW | 44.679° | 2026-05-10 06:01:44.709Z | 196.34° SSW |
| 4 mins | 2026-05-10 16:30:44.709Z | 114.932° SE | 2026-05-10 16:32:44.709Z | 55.282° ENE | 25.747° | 2026-05-10 16:34:44.709Z | 15.323° NNE |
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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