OBJECT XM, 65733 (Decayed)
Orbit data source: Space-Track
OBJECT XM, 65733 was a Japanese 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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65733 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 XM
1 65733U 98067XM 26020.92375749 .09795873 12158-4 14287-2 0 9993
2 65733 51.6117 289.2886 0004779 208.5099 151.5664 16.33783644 19418Epoch: 2026-01-20T22:10Z
TLE epoch observation values (Epoch: 2026-01-20T22:10:12.647Z)
Latitude
-0.00001°
Longitude
-163.56276°
Altitude
185.913 km
Speed
7.795 km/s
True Right ascension
19h 17m 09s
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
18:57:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
186.057 km
Perigee altitude
179.786 km
Semi-major axis
6,561.059 km
Eccentricity
0.00048
Inclination
51.6117°
RAAN
289.2886°
Arg. of periapsis
208.5099°
True anomaly
151.59246°
Mean anomaly
151.5664°
Eccentric anomaly
151.57943°
Mean motion
4.08397 °/min
Orbital period
88.15 mins
BSTAR
0.0014287
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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 XM 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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