OBJECT H, 59058 (Decayed)
Orbit data source: Space-Track
OBJECT H, 59058 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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59058 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 H
1 59058U 24039H 25127.99152363 .09389883 26089-5 82448-3 0 9997
2 59058 97.3962 104.6898 0009242 210.9051 149.1705 16.39206788 66892Epoch: 2025-05-07T23:47Z
TLE epoch observation values (Epoch: 2025-05-07T23:47:47.641Z)
Latitude
-0.00005°
Longitude
-118.32713°
Altitude
176.362 km
Speed
7.797 km/s
True Right ascension
06h 58m 45s
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
19:40:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
170.769 km
Perigee altitude
158.675 km
Semi-major axis
6,542.859 km
Eccentricity
0.00092
Inclination
97.3962°
RAAN
104.6898°
Arg. of periapsis
210.9051°
True anomaly
149.22472°
Mean anomaly
149.1705°
Eccentric anomaly
149.19762°
Mean motion
4.10102 °/min
Orbital period
87.78 mins
BSTAR
0.00082448
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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 H 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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