OBJECT BP, 58317 (Decayed)
Orbit data source: Space-Track
OBJECT BP, 58317 was a satellite in LEO that was launched on Sat, 11 Nov 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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58317 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT BP
1 58317U 23174BP 25091.62106398 .07821529 24928-5 14590-2 0 9998
2 58317 97.3838 180.0067 0013270 269.4347 90.5427 16.31943736 78302Epoch: 2025-04-01T14:54Z
TLE epoch observation values (Epoch: 2025-04-01T14:54:19.927Z)
Latitude
-0.00011°
Longitude
126.2037°
Altitude
190.657 km
Speed
7.792 km/s
True Right ascension
12h 00m 01s
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
04:16:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
192.847 km
Perigee altitude
175.431 km
Semi-major axis
6,562.276 km
Eccentricity
0.00133
Inclination
97.3838°
RAAN
180.0067°
Arg. of periapsis
269.4347°
True anomaly
90.69475°
Mean anomaly
90.5427°
Eccentric anomaly
90.61873°
Mean motion
4.08283 °/min
Orbital period
88.17 mins
BSTAR
0.001459
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Other satellites on launch #174 in the year 2023 (2023-11-11 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 BP 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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