OBJECT N, 59063 (Decayed)
Orbit data source: Space-Track
OBJECT N, 59063 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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59063 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 N
1 59063U 24039N 25123.19697148 .15262011 26408-5 23866-3 0 9990
2 59063 97.3867 99.9366 0010702 236.9191 123.1086 16.47867169 66163Epoch: 2025-05-03T04:43Z
TLE epoch observation values (Epoch: 2025-05-03T04:43:38.335Z)
Latitude
-0.00002°
Longitude
167.68418°
Altitude
152.04 km
Speed
7.813 km/s
True Right ascension
06h 39m 44s
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
02:42:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
148.732 km
Perigee altitude
134.777 km
Semi-major axis
6,519.892 km
Eccentricity
0.00107
Inclination
97.3867°
RAAN
99.9366°
Arg. of periapsis
236.9191°
True anomaly
123.21125°
Mean anomaly
123.1086°
Eccentric anomaly
123.15993°
Mean motion
4.12271 °/min
Orbital period
87.32 mins
BSTAR
0.00023866
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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 N 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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