OBJECT AE, 101139
Orbit data source: Space-Track
OBJECT AE, 101139 is a satellite in LEO that was launched on Tue, 20 Oct 2026 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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101139 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OBJECT AE
1 A1139U 26237AE 26297.25002315 -.00024391 00000-0 -23363-2 0 9998
2 A1139 52.9880 306.1926 0005724 265.3724 75.0400 14.92508103 1305Epoch: 2026-10-24T06:00Z
TLE epoch observation values (Epoch: 2026-10-24T06:00:02.000Z)
Latitude
-15.63938°
Longitude
171.40907°
Altitude
593.278 km
Speed
7.564 km/s
True Right ascension
19h 36m 18s
True Declination
-15° 32' 54"
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
08:07:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.387 km
Perigee altitude
586.409 km
Semi-major axis
6,968.535 km
Eccentricity
0.00057
Inclination
52.988°
RAAN
306.1926°
Arg. of periapsis
265.3724°
True anomaly
75.10338°
Mean anomaly
75.04°
Eccentric anomaly
75.07169°
Mean motion
3.73105 °/min
Orbital period
96.49 mins
BSTAR
-0.0023363
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Other satellites on launch #237 in the year 2026 (2026-10-20 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-25 03:08:45.211Z | 216.367° SW | 2026-10-25 03:12:45.211Z | 109.007° ESE | 61.979° | 2026-10-25 03:16:45.211Z | 55.474° ENE |
| 6 mins | 2026-10-25 04:50:45.211Z | 287.895° WNW | 2026-10-25 04:52:45.211Z | 323.966° NNW | 26.873° | 2026-10-25 04:56:45.211Z | 32.482° NE |
| 5 mins | 2026-10-25 08:14:45.211Z | 343.836° N | 2026-10-25 08:16:45.211Z | 17.835° NNE | 20.206° | 2026-10-25 08:19:45.211Z | 63.828° ENE |
| 7 mins | 2026-10-25 09:54:45.211Z | 316.424° NNW | 2026-10-25 09:57:45.211Z | 21.141° NNE | 68.116° | 2026-10-25 10:01:45.211Z | 120.611° SE |
| 4 mins | 2026-10-25 11:36:45.211Z | 254.48° W | 2026-10-25 11:37:45.211Z | 237.576° WSW | 17.922° | 2026-10-25 11:40:45.211Z | 192.492° SSW |
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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