DECAYED

OBJECT AH, 52425 (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 AH, 52425 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
52425, 2022-047AH
Orbit
Decayed
Country
Flag of TBDTBD
Related 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)
2022-05-02 (3 years ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.126 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 year ago

TLE from 1 year ago
0 OBJECT AH
1 52425U 22047AH  24220.38791822  .09950694  25075-5  11309-2 0  9995
2 52425  97.3633 315.2486 0014929 267.1874  92.7715 16.36640179127969
Epoch: 2024-08-07T09:18Z
TLE epoch observation values (Epoch: 2024-08-07T09:18:36.134Z)
Latitude
-0.00001°
Longitude
-140.79371°
Altitude
178.491 km
Speed
7.799 km/s
True Right ascension
21h 00m 59s
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
13:20:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
181.344 km
Perigee altitude
161.788 km
Semi-major axis
6,549.703 km
Eccentricity
0.00149
Inclination
97.3633°
RAAN
315.2486°
Arg. of periapsis
267.1874°
True anomaly
92.94236°
Mean anomaly
92.7715°
Eccentric anomaly
92.85693°
Mean motion
4.09459 °/min
Orbital period
87.92 mins
BSTAR
0.0011309
Loading maneuver chart data...
Computing Atmospheric mass density...

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