OBJECT AJ, 52426 (Decayed)
Orbit data source: Space-Track
OBJECT AJ, 52426 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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52426 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Cyl + Box, 0.7 m
Radar Cross Section
2.660 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT AJ
1 52426U 22047AJ 25019.00528027 .15878001 25434-5 29627-3 0 9997
2 52426 97.3404 120.4801 0013613 276.1677 83.8075 16.46499169153212Epoch: 2025-01-19T00:07Z
TLE epoch observation values (Epoch: 2025-01-19T00:07:36.215Z)
Latitude
-0.00001°
Longitude
-0.06722°
Altitude
150.886 km
Speed
7.816 km/s
True Right ascension
08h 01m 55s
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
21:21:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
154.248 km
Perigee altitude
136.487 km
Semi-major axis
6,523.504 km
Eccentricity
0.00136
Inclination
97.3404°
RAAN
120.4801°
Arg. of periapsis
276.1677°
True anomaly
83.96261°
Mean anomaly
83.8075°
Eccentric anomaly
83.88505°
Mean motion
4.11928 °/min
Orbital period
87.39 mins
BSTAR
0.00029627
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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 AJ 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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