OBJECT F, 59056 (Decayed)
Orbit data source: Space-Track
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Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT F, 59056 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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59056 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
Manufacturer
Sputniks
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 OBJECT F
1 59056U 24039F 25126.89772039 .07301363 25664-5 98490-3 0 9998
2 59056 97.3883 103.5483 0008539 203.6382 156.4524 16.35337833 66728Epoch: 2025-05-06T21:32Z
TLE epoch observation values (Epoch: 2025-05-06T21:32:43.041Z)
Latitude
-0.00002°
Longitude
-84.62136°
Altitude
186.614 km
Speed
7.791 km/s
True Right ascension
06h 54m 11s
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
13:59:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
180.643 km
Perigee altitude
169.451 km
Semi-major axis
6,553.184 km
Eccentricity
0.00085
Inclination
97.3883°
RAAN
103.5483°
Arg. of periapsis
203.6382°
True anomaly
156.49145°
Mean anomaly
156.4524°
Eccentric anomaly
156.47193°
Mean motion
4.09133 °/min
Orbital period
87.99 mins
BSTAR
0.0009849
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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 F 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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