OBJECT XX, 66911
Orbit data source: Space-Track
OBJECT XX, 66911 is 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.
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66911 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 OBJECT XX
1 66911U 98067XX 26100.47401911 .03277748 11857-4 16574-2 0 9998
2 66911 51.6062 257.2206 0014018 301.0012 58.9628 16.19642199 20244Epoch: 2026-04-10T11:22Z
TLE epoch observation values (Epoch: 2026-04-10T11:22:35.251Z)
Latitude
-0.00004°
Longitude
-112.13347°
Altitude
216.524 km
Speed
7.781 km/s
True Right ascension
17h 08m 52s
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
03:03:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
230.303 km
Perigee altitude
211.801 km
Semi-major axis
6,599.189 km
Eccentricity
0.0014
Inclination
51.6062°
RAAN
257.2206°
Arg. of periapsis
301.0012°
True anomaly
59.10056°
Mean anomaly
58.9628°
Eccentric anomaly
59.03167°
Mean motion
4.04862 °/min
Orbital period
88.92 mins
BSTAR
0.0016574
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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 XX 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. |
|---|---|---|---|---|---|---|---|
| OBJECT XX 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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