OBJECT B, 69793
Orbit data source: Space-Track
OBJECT B, 69793 is an American satellite in LEO that was launched on Fri, 03 Jul 2026 UTC launched from the Kwajalein (KWAJL). 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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69793 intel report (Beta)
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USExpand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OBJECT B
1 69793U 26152B 26185.35315480 .00019114 00000-0 18294-3 0 9994
2 69793 20.5986 50.6800 0023016 201.8951 158.0512 15.63830603 156Epoch: 2026-07-04T08:28Z
TLE epoch observation values (Epoch: 2026-07-04T08:28:32.574Z)
Latitude
-0°
Longitude
1.17621°
Altitude
388.58 km
Speed
7.672 km/s
True Right ascension
03h 22m 43s
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
07:58:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
397.48 km
Perigee altitude
366.362 km
Semi-major axis
6,760.058 km
Eccentricity
0.0023
Inclination
20.5986°
RAAN
50.68°
Arg. of periapsis
201.8951°
True anomaly
158.14952°
Mean anomaly
158.0512°
Eccentric anomaly
158.10039°
Mean motion
3.90497 °/min
Orbital period
92.19 mins
BSTAR
0.00018294
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Other satellites on launch #152 in the year 2026 (2026-07-03 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 B Visibility
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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. |
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| OBJECT B is likely not visible in the next few days. |
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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