OBJECT P, 59064 (Decayed)
Orbit data source: Space-Track
OBJECT P, 59064 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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59064 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 OBJECT P
1 59064U 24039P 26002.21265238 .08351156 26974-5 79667-3 0 9991
2 59064 97.4059 353.4172 0001300 208.5179 151.6048 16.38661712104080Epoch: 2026-01-02T05:06Z
TLE epoch observation values (Epoch: 2026-01-02T05:06:13.165Z)
Latitude
-0.00011°
Longitude
175.00625°
Altitude
173.363 km
Speed
7.802 km/s
True Right ascension
23h 33m 40s
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
04:23:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.025 km
Perigee altitude
165.324 km
Semi-major axis
6,544.312 km
Eccentricity
0.00013
Inclination
97.4059°
RAAN
353.4172°
Arg. of periapsis
208.5179°
True anomaly
151.61188°
Mean anomaly
151.6048°
Eccentric anomaly
151.60834°
Mean motion
4.09965 °/min
Orbital period
87.81 mins
BSTAR
0.00079667
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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 P 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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