BANE, 58465
Orbit data source: Space-Track
BANE, 58465 is a payload satellite owned by York Space Sys (US) in SSO that was launched on Fri, 01 Dec 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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58465 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
York Space Sys
Mission
Operational Commercial Technology
Bus & Motor
S-CLASS, Unknown motor
Mass
~150 kg wet, ~150 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 1.0 m
Radar Cross Section
1.244 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 BANE
1 58465U 23185D 25306.54387586 .00044279 00000-0 78370-3 0 9993
2 58465 97.3659 19.8287 0003938 280.6532 79.4276 15.50167938107292Epoch: 2025-11-02T13:03Z
TLE epoch observation values (Epoch: 2025-11-02T13:03:10.874Z)
Latitude
-0.00001°
Longitude
141.97531°
Altitude
418.878 km
Speed
7.66 km/s
True Right ascension
01h 19m 18s
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
23:58:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
415.834 km
Perigee altitude
410.485 km
Semi-major axis
6,791.296 km
Eccentricity
0.00039
Inclination
97.3659°
RAAN
19.8287°
Arg. of periapsis
280.6532°
True anomaly
79.47196°
Mean anomaly
79.4276°
Eccentric anomaly
79.44978°
Mean motion
3.87806 °/min
Orbital period
92.83 mins
BSTAR
0.0007837
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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.BANE Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-03 04:41:01.146Z | 138.09° SSE | 2025-11-03 04:43:01.146Z | 91.163° ESE | 30.352° | 2025-11-03 04:46:01.146Z | 7.124° NNE |
| 4 mins | 2025-11-03 17:31:01.146Z | 45.231° ENE | 2025-11-03 17:33:01.146Z | 119.734° SE | 29.408° | 2025-11-03 17:35:01.146Z | 163.709° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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