OBJECT XD, 62297 (Decayed)
Orbit data source: Space-Track
OBJECT XD, 62297 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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62297 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT XD
1 62297U 98067XD 25064.26411513 .04593247 11898-4 22015-2 0 9993
2 62297 51.6147 89.8286 0005059 24.8961 335.2301 16.20565003 13483Epoch: 2025-03-05T06:20Z
TLE epoch observation values (Epoch: 2025-03-05T06:20:19.547Z)
Latitude
0.00003°
Longitude
-168.5085°
Altitude
215.749 km
Speed
7.78 km/s
True Right ascension
05h 59m 18s
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
07:50:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
221.883 km
Perigee altitude
215.208 km
Semi-major axis
6,596.683 km
Eccentricity
0.00051
Inclination
51.6147°
RAAN
89.8286°
Arg. of periapsis
24.8961°
True anomaly
335.2058°
Mean anomaly
335.2301°
Eccentric anomaly
335.21795°
Mean motion
4.05093 °/min
Orbital period
88.87 mins
BSTAR
0.0022015
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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 XD 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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