OBJECT AE, 100911
Orbit data source: Space-Track
OBJECT AE, 100911 is a satellite in SSO that was launched on Thu, 01 Oct 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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100911 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: 12 hours ago
TLE from 12 hours ago
0 OBJECT AE
1 A0911U 26227AE 26281.60838797 .00007026 00000-0 35940-3 0 9996
2 A0911 97.4471 351.0044 0001417 87.3674 272.7721 15.16943364 1045Epoch: 2026-10-08T14:36Z
TLE epoch observation values (Epoch: 2026-10-08T14:36:04.720Z)
Latitude
-0.00009°
Longitude
114.74297°
Altitude
518.123 km
Speed
7.604 km/s
True Right ascension
23h 24m 01s
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
20:36:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.033 km
Perigee altitude
511.08 km
Semi-major axis
6,890.194 km
Eccentricity
0.00014
Inclination
97.4471°
RAAN
351.0044°
Arg. of periapsis
87.3674°
True anomaly
272.75588°
Mean anomaly
272.7721°
Eccentric anomaly
272.76399°
Mean motion
3.79486 °/min
Orbital period
94.87 mins
BSTAR
0.0003594
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Other satellites on launch #227 in the year 2026 (2026-10-01 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 | 2026-10-09 04:58:37.776Z | 179.537° S | 2026-10-09 05:01:37.776Z | 278.434° WNW | 62.875° | 2026-10-09 05:04:37.776Z | 340.23° N |
| 5 mins | 2026-10-09 18:05:37.776Z | 339.496° N | 2026-10-09 18:07:37.776Z | 275.353° WNW | 38.445° | 2026-10-09 18:10:37.776Z | 218.934° 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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