FALCONSAT-10, 58291
Orbit data source: Space-Track
FALCONSAT-10, 58291 is a payload satellite owned by USAF Academy (US) in SSO that was launched on Sat, 11 Nov 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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58291 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
USAF Academy
Mission
Operational Defense Technology
Bus & Motor
FALCONSAT, Unknown motor
Mass
140 kg wet, 140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.7 m
Radar Cross Section
0.780 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 FALCONSAT-10
1 58291U 23174AM 26285.17829793 .00005381 00000-0 19602-3 0 9999
2 58291 97.3710 0.0545 0009564 127.4100 232.8012 15.28578132162635Epoch: 2026-10-12T04:16Z
TLE epoch observation values (Epoch: 2026-10-12T04:16:44.941Z)
Latitude
0.00002°
Longitude
-84.89321°
Altitude
487.135 km
Speed
7.619 km/s
True Right ascension
00h 00m 13s
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
22:03:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.571 km
Perigee altitude
470.459 km
Semi-major axis
6,855.152 km
Eccentricity
0.00096
Inclination
97.371°
RAAN
0.0545°
Arg. of periapsis
127.41°
True anomaly
232.71397°
Mean anomaly
232.8012°
Eccentric anomaly
232.75758°
Mean motion
3.824 °/min
Orbital period
94.14 mins
BSTAR
0.00019602
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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.FALCONSAT-10 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 | 2026-10-13 05:33:04.359Z | 197.021° SSW | 2026-10-13 05:35:04.359Z | 249.62° W | 41.85° | 2026-10-13 05:38:04.359Z | 330.083° NNW |
| 5 mins | 2026-10-13 18:33:04.359Z | 341.157° N | 2026-10-13 18:35:04.359Z | 293.193° NW | 30.737° | 2026-10-13 18:38:04.359Z | 226.962° WSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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