OBJECT AF, 52423 (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 AF, 52423 was a satellite in LEO that was launched on Mon, 02 May 2022 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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52423 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
E-Space
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 6U?, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.126 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 OBJECT AF
1 52423U 22047AF 24285.98978330 .04187927 25232-5 17414-3 0 9996
2 52423 97.3405 18.6825 0011355 271.9448 88.0553 16.42611819137892Epoch: 2024-10-11T23:45Z
TLE epoch observation values (Epoch: 2024-10-11T23:45:17.277Z)
Latitude
0.00005°
Longitude
1.30845°
Altitude
161.877 km
Speed
7.809 km/s
True Right ascension
01h 14m 43s
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
13:25:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
163.085 km
Perigee altitude
148.246 km
Semi-major axis
6,533.802 km
Eccentricity
0.00114
Inclination
97.3405°
RAAN
18.6825°
Arg. of periapsis
271.9448°
True anomaly
88.18535°
Mean anomaly
88.0553°
Eccentric anomaly
88.12032°
Mean motion
4.10955 °/min
Orbital period
87.6 mins
BSTAR
0.00017414
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Other satellites on launch #47 in the year 2022 (2022-05-02 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 AF 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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