DECAYED

OBJECT AJ, 52426 (Decayed)

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 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.

Not visible in the next 10 days
Identifier
52426, 2022-047AJ
Orbit
Decayed
Country
Flag of TBDTBD
Related business
None
Manufacturer
Astrix
Mission
Decayed Commercial Technology
Bus & Motor
CUBESAT 1U?, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2022-05-02 (3 years ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 months ago

TLE from 8 months 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 16.46499169153212
Epoch: 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
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
13:20:07
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
Loading maneuver chart data...
Computing Atmospheric mass density...

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