FACSAT-2, 56205 (Decayed)
Orbit data source: Space-Track
FACSAT-2, 56205 was a payload satellite owned by EMAVI (CO) in LEO that was launched on Sat, 15 Apr 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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56205 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CO / COLRelated business
Manufacturer
GOMSpace
Mission
Decayed Defense Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.3 m
Radar Cross Section
0.211 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 FACSAT-2
1 56205U 23054AD 25300.42042571 .09741927 26127-5 82939-3 0 9993
2 56205 97.2857 219.0983 0005678 177.9723 182.1600 16.39589118143537Epoch: 2025-10-27T10:05Z
TLE epoch observation values (Epoch: 2025-10-27T10:05:24.781Z)
Latitude
-0.00007°
Longitude
31.72253°
Altitude
173.864 km
Speed
7.8 km/s
True Right ascension
14h 36m 23s
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
07:41:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.413 km
Perigee altitude
159.984 km
Semi-major axis
6,541.836 km
Eccentricity
0.00057
Inclination
97.2857°
RAAN
219.0983°
Arg. of periapsis
177.9723°
True anomaly
182.15755°
Mean anomaly
182.16°
Eccentric anomaly
182.15877°
Mean motion
4.10198 °/min
Orbital period
87.76 mins
BSTAR
0.00082939
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Other satellites on launch #54 in the year 2023 (2023-04-15 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.FACSAT-2 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
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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