DECAYED

OBJECT AJ, 47445 (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, 47445 was a satellite in LEO that was launched on Sun, 24 Jan 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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
OBJECT AJ details
Identifier
47445, 2021-006AJ
Orbit
Decayed
Last TLE update1 month ago
Origin
Flag of TBDTU Dresden (TBD)
ManufacturerTU Dresden
MissionDecayed Amateur Science
Bus & MotorCUBESAT 2U, Unknown motor
Mass2 kg wet, 2 kg dry
Launch date (UTC)
2021-01-24 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object typeUnknown
Shape & HBRBox, Unknown HBR
Radar Cross Section0.025 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 1 month ago
0 OBJECT AJ
1 47445U 21006AJ  24320.07680123  .17272437  25045-5  27578-3 0  9997
2 47445  97.2621  23.7910 0008960 269.2652  90.7625 16.47927372212215
Epoch: 2024-11-15T01:50Z
Definitive object data (Epoch: 2024-11-15T01:50:35.626Z)
Latitude-0.00005°
Longitude-58.50728°
Altitude148.148 km
Speed7.817 km/s
True Right ascension01h 35m 09s
True Declination0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.
Orbital elements
Apogee altitude147.432 km
Perigee altitude135.749 km
Semi-major axis6,519.727 km
Eccentricity0.000896
Inclination97.2621°
RAAN23.791°
Arg. of periapsis269.2652°
True anomaly90.86516°
Mean anomaly90.7625°
Eccentric anomaly90.81383°
Mean motion4.12286 °/min
BSTAR0.00027578
Orbital period87.32 mins
Loading maneuver chart data...

OBJECT AJ Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
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.
|