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: 16 hours ago
TLE from 16 hours ago
0 BANE
1 58465U 23185D 25261.29077848 .00029535 00000-0 61373-3 0 9995
2 58465 97.3720 333.7267 0006989 99.0438 261.1602 15.45596919100298Epoch: 2025-09-18T06:58Z
TLE epoch observation values (Epoch: 2025-09-18T06:58:43.26Z)
Latitude
-0.00006°
Longitude
-128.40803°
Altitude
433.485 km
Speed
7.651 km/s
True Right ascension
22h 14m 54s
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
15:24:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.311 km
Perigee altitude
421.799 km
Semi-major axis
6,804.692 km
Eccentricity
0.0007
Inclination
97.372°
RAAN
333.7267°
Arg. of periapsis
99.0438°
True anomaly
261.08107°
Mean anomaly
261.1602°
Eccentric anomaly
261.12064°
Mean motion
3.86661 °/min
Orbital period
93.1 mins
BSTAR
0.00061373
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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 | 2025-09-19 04:51:40.634Z | 159.597° S | 2025-09-19 04:54:40.634Z | 33.107° NE | 42.11° | 2025-09-19 04:56:40.634Z | 354.684° N |
| 5 mins | 2025-09-19 17:43:40.634Z | 17.217° NNE | 2025-09-19 17:45:40.634Z | 64.041° ENE | 43.669° | 2025-09-19 17:48:40.634Z | 187.532° SSW |
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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