OBJECT K, 58471 (Decayed)
Orbit data source: Space-Track
OBJECT K, 58471 was a satellite in LEO that was launched on Fri, 01 Dec 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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58471 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
BAZOOMQ Space Research Lab (AM)Manufacturer
NPUA/BAZMQ
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 OBJECT K
1 58471U 23185K 25114.86339687 .10095164 24939-5 11708-2 0 9994
2 58471 97.3435 194.4543 0015215 263.2900 96.6666 16.36438907 78320Epoch: 2025-04-24T20:43Z
TLE epoch observation values (Epoch: 2025-04-24T20:43:17.489Z)
Latitude
-0.00005°
Longitude
30.50271°
Altitude
179.714 km
Speed
7.798 km/s
True Right ascension
12h 57m 49s
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
12:03:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
182.069 km
Perigee altitude
162.136 km
Semi-major axis
6,550.239 km
Eccentricity
0.00152
Inclination
97.3435°
RAAN
194.4543°
Arg. of periapsis
263.29°
True anomaly
96.83973°
Mean anomaly
96.6666°
Eccentric anomaly
96.75317°
Mean motion
4.09409 °/min
Orbital period
87.93 mins
BSTAR
0.0011708
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Other satellites on launch #185 in the year 2023 (2023-12-01 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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