DECAYED

OBJECT-DD, 55108 (Decayed)

Orbit data source: Space-Track

OBJECT-DD, 55108 was a satellite in LEO that was launched on Tue, 03 Jan 2023 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
Identifier
55108, 2023-001DD
Orbit
Decayed
Country
Flag of TBDTBD
Related business
None
Manufacturer
Unknown
Mission
Decayed Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2023-01-03 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

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

TLE from 8 months ago
0 OBJECT-DD
1 55108U 23001DD  25036.82836087  .03978260  24109-5  16780-2 0  9993
2 55108  97.3571 111.2551 0006989 291.2913  68.7631 16.22931529116962
Epoch: 2025-02-05T19:52Z
TLE epoch observation values (Epoch: 2025-02-05T19:52:50.379Z)
Latitude
Longitude
36.83149°
Altitude
213.169 km
Speed
7.78 km/s
True Right ascension
07h 25m 01s
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
13:23:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
213.036 km
Perigee altitude
203.829 km
Semi-major axis
6,586.569 km
Eccentricity
0.0007
Inclination
97.3571°
RAAN
111.2551°
Arg. of periapsis
291.2913°
True anomaly
68.83777°
Mean anomaly
68.7631°
Eccentric anomaly
68.80043°
Mean motion
4.06026 °/min
Orbital period
88.66 mins
BSTAR
0.001678
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|