OBJECT K, 59060 (Decayed)
Orbit data source: Space-Track
OBJECT K, 59060 was a satellite in LEO that was launched on Thu, 29 Feb 2024 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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59060 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 OBJECT K
1 59060U 24039K 25133.32764041 .15065791 26402-5 17718-3 0 9999
2 59060 97.3885 110.3756 0012027 230.2391 129.7854 16.49499424 67738Epoch: 2025-05-13T07:51Z
TLE epoch observation values (Epoch: 2025-05-13T07:51:48.131Z)
Latitude
-0.0001°
Longitude
121.09711°
Altitude
148.942 km
Speed
7.814 km/s
True Right ascension
07h 21m 30s
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
04:24:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
145.285 km
Perigee altitude
129.613 km
Semi-major axis
6,515.586 km
Eccentricity
0.0012
Inclination
97.3885°
RAAN
110.3756°
Arg. of periapsis
230.2391°
True anomaly
129.8912°
Mean anomaly
129.7854°
Eccentric anomaly
129.83831°
Mean motion
4.1268 °/min
Orbital period
87.23 mins
BSTAR
0.00017718
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Other satellites on launch #39 in the year 2024 (2024-02-29 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 K 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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