OBJECT XL, 65732 (Decayed)
Orbit data source: Space-Track
OBJECT XL, 65732 was a satellite owned by Ryman Sat (JP) 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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65732 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 OBJECT XL
1 65732U 98067XL 26047.27951905 .10199253 12460-4 79249-3 0 9991
2 65732 51.6061 154.7117 0006246 319.9198 40.1367 16.39378610 23558Epoch: 2026-02-16T06:42Z
TLE epoch observation values (Epoch: 2026-02-16T06:42:30.445Z)
Latitude
-0.00001°
Longitude
-92.19131°
Altitude
165.097 km
Speed
7.81 km/s
True Right ascension
10h 18m 50s
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
15:42:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
172.077 km
Perigee altitude
163.9 km
Semi-major axis
6,546.126 km
Eccentricity
0.00062
Inclination
51.6061°
RAAN
154.7117°
Arg. of periapsis
319.9198°
True anomaly
40.18287°
Mean anomaly
40.1367°
Eccentric anomaly
40.15978°
Mean motion
4.09795 °/min
Orbital period
87.85 mins
BSTAR
0.00079249
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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 XL 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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