OBJECT XU, 66908 (Decayed)
Orbit data source: Space-Track
OBJECT XU, 66908 was an American satellite in LEO that was delivered to and deployed from the ISS. 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. This object's orbit decayed before it could be identified.
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66908 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 OBJECT XU
1 66908U 98067XU 26127.21805227 .03226817 11977-4 11668-2 0 9996
2 66908 51.6088 120.0031 0001220 14.1359 345.9695 16.24076855 24465Epoch: 2026-05-07T05:13Z
TLE epoch observation values (Epoch: 2026-05-07T05:13:59.716Z)
Latitude
0.00002°
Longitude
176.43695°
Altitude
208.488 km
Speed
7.783 km/s
True Right ascension
08h 00m 00s
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
00:14:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
209.839 km
Perigee altitude
208.231 km
Semi-major axis
6,587.172 km
Eccentricity
0.00012
Inclination
51.6088°
RAAN
120.0031°
Arg. of periapsis
14.1359°
True anomaly
345.96611°
Mean anomaly
345.9695°
Eccentric anomaly
345.96781°
Mean motion
4.05971 °/min
Orbital period
88.68 mins
BSTAR
0.0011668
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Other satellites on launch #67 in the year 1998 (1998-11-20 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 XU 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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| This satellite is decayed. |
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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