Showing default

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.

Loading next visibility...
Identifier
58291, 2023-174AM
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
USAF Academy
Mission
Operational Defense Technology
Bus & Motor
FALCONSAT, Unknown motor
Mass
140 kg wet, 140 kg dry
Launch date (UTC)
2023-11-11 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.5 m
Radar Cross Section
0.780 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 FALCONSAT-10
1 58291U 23174AM  26126.49953771  .00004838  00000-0  18350-3 0  9997
2 58291  97.3806 202.9766 0007786 346.2759  13.8267 15.27309403138403
Epoch: 2026-05-06T11:59Z
TLE epoch observation values (Epoch: 2026-05-06T11:59:20.058Z)
Latitude
-0.00003°
Longitude
158.78388°
Altitude
481.772 km
Speed
7.627 km/s
True Right ascension
13h 31m 54s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
08:28:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.155 km
Perigee altitude
475.474 km
Semi-major axis
6,858.951 km
Eccentricity
0.00078
Inclination
97.3806°
RAAN
202.9766°
Arg. of periapsis
346.2759°
True anomaly
13.84804°
Mean anomaly
13.8267°
Eccentric anomaly
13.83737°
Mean motion
3.82082 °/min
Orbital period
94.22 mins
BSTAR
0.0001835
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|