OBJECT P, 59064
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT P, 59064 is a satellite in SSO 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.
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59064 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
Manufacturer
Sputniks
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 OBJECT P
1 59064U 24039P 25272.27170220 .00123803 00000-0 10675-2 0 9999
2 59064 97.4306 250.3098 0003329 0.8913 359.2354 15.68872633 89041Epoch: 2025-09-29T06:31Z
TLE epoch observation values (Epoch: 2025-09-29T06:31:15.070Z)
Latitude
0.00003°
Longitude
144.2192°
Altitude
363.035 km
Speed
7.693 km/s
True Right ascension
16h 41m 14s
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
14:03:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
361.269 km
Perigee altitude
356.783 km
Semi-major axis
6,737.163 km
Eccentricity
0.00033
Inclination
97.4306°
RAAN
250.3098°
Arg. of periapsis
0.8913°
True anomaly
359.23489°
Mean anomaly
359.2354°
Eccentric anomaly
359.23515°
Mean motion
3.92489 °/min
Orbital period
91.72 mins
BSTAR
0.0010675
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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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| OBJECT P is likely not visible in the next few days. |
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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