DECAYED

OBJECT K, 56941 (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 K, 56941 was a satellite in LEO that was launched on Mon, 12 Jun 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
56941, 2023-084K
Orbit
Decayed
Country
Flag of TBDTBD
Related business
None
Manufacturer
Unknown
Mission
Decayed Commercial Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2023-06-12 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.006 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 9 months ago

TLE from 9 months ago
0 OBJECT K
1 56941U 23084K   25024.33266643  .10961626  25861-5  10399-2 0  9990
2 56941  97.5144 161.3546 0011670 293.6899  66.3174 16.38425087 90510
Epoch: 2025-01-24T07:59Z
TLE epoch observation values (Epoch: 2025-01-24T07:59:02.379Z)
Latitude
-0.00005°
Longitude
-82.30266°
Altitude
170.178 km
Speed
7.806 km/s
True Right ascension
10h 45m 25s
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
11:16:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
174.448 km
Perigee altitude
159.172 km
Semi-major axis
6,544.947 km
Eccentricity
0.00117
Inclination
97.5144°
RAAN
161.3546°
Arg. of periapsis
293.6899°
True anomaly
66.43994°
Mean anomaly
66.3174°
Eccentric anomaly
66.37866°
Mean motion
4.09906 °/min
Orbital period
87.83 mins
BSTAR
0.0010399
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|