OBJECT K, 56941 (Decayed)
Orbit data source: Space-Track
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.
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56941 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
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 & historyLast TLE update: 1 year ago
TLE from 1 year 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 90510Epoch: 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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
03:16:16
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
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Other satellites on launch #84 in the year 2023 (2023-06-12 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT K Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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