OBJECT AE, 69008
Orbit data source: Space-Track
OBJECT AE, 69008 is a satellite in SSO that was launched on Sun, 03 May 2026 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.
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69008 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
Unknown
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 OBJECT AE
1 69008U 26100AE 26130.17682146 .00001039 00000-0 11010-3 0 9998
2 69008 97.7384 28.3329 0002143 287.1432 72.9552 14.91196974 1021Epoch: 2026-05-10T04:14Z
TLE epoch observation values (Epoch: 2026-05-10T04:14:37.374Z)
Latitude
0.00002°
Longitude
96.69352°
Altitude
596.806 km
Speed
7.562 km/s
True Right ascension
01h 53m 19s
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
20:32:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.714 km
Perigee altitude
589.727 km
Semi-major axis
6,969.358 km
Eccentricity
0.00021
Inclination
97.7384°
RAAN
28.3329°
Arg. of periapsis
287.1432°
True anomaly
72.97868°
Mean anomaly
72.9552°
Eccentric anomaly
72.96694°
Mean motion
3.73039 °/min
Orbital period
96.5 mins
BSTAR
0.0001101
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Other satellites on launch #100 in the year 2026 (2026-05-03 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 | 2026-05-10 17:14:31.410Z | 168.755° S | 2026-05-10 17:18:31.410Z | 299.942° NW | 44.737° | 2026-05-10 17:22:31.410Z | 346.389° N |
| 6 mins | 2026-05-11 06:35:31.410Z | 343.403° N | 2026-05-11 06:37:31.410Z | 294.414° NW | 32.453° | 2026-05-11 06:41:31.410Z | 219.013° SW |
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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