OBJECT L, 59061 (Decayed)
Orbit data source: Space-Track
OBJECT L, 59061 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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59061 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 L
1 59061U 24039L 25124.14560288 .11249086 26374-5 51333-3 0 9993
2 59061 97.3842 100.7726 0008771 219.5766 140.4895 16.42537515 66303Epoch: 2025-05-04T03:29Z
TLE epoch observation values (Epoch: 2025-05-04T03:29:40.088Z)
Latitude
-0.00009°
Longitude
-173.92213°
Altitude
166.743 km
Speed
7.803 km/s
True Right ascension
06h 43m 05s
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
02:38:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.596 km
Perigee altitude
150.134 km
Semi-major axis
6,534.002 km
Eccentricity
0.00088
Inclination
97.3842°
RAAN
100.7726°
Arg. of periapsis
219.5766°
True anomaly
140.55339°
Mean anomaly
140.4895°
Eccentric anomaly
140.52145°
Mean motion
4.10936 °/min
Orbital period
87.6 mins
BSTAR
0.00051333
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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 L 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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