OBJECT XE, 62298 (Decayed)
Orbit data source: Space-Track
OBJECT XE, 62298 was a satellite owned by Chiba kogyu (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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62298 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 OBJECT XE
1 62298U 98067XE 25089.55016338 .06907718 12136-4 12698-2 0 9995
2 62298 51.6023 320.8807 0008675 257.8161 102.1891 16.31399071 17459Epoch: 2025-03-30T13:12Z
TLE epoch observation values (Epoch: 2025-03-30T13:12:14.116Z)
Latitude
0.00006°
Longitude
-65.35687°
Altitude
190.753 km
Speed
7.793 km/s
True Right ascension
21h 23m 31s
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
01:02:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
195.012 km
Perigee altitude
183.617 km
Semi-major axis
6,567.451 km
Eccentricity
0.00087
Inclination
51.6023°
RAAN
320.8807°
Arg. of periapsis
257.8161°
True anomaly
102.28624°
Mean anomaly
102.1891°
Eccentric anomaly
102.23767°
Mean motion
4.07801 °/min
Orbital period
88.28 mins
BSTAR
0.0012698
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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 XE 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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