SUCHAI-3, 52191 (Decayed)
Orbit data source: Space-Track
SUCHAI-3, 52191 was a payload satellite owned by SPEL/UCH (CL) in LEO that was launched on Fri, 01 Apr 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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52191 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / CHLERelated business
Space and Planetary Exploration Lab, University of Chile (CL)Manufacturer
SPEL/UCH
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~4 kg wet, ~4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 SUCHAI-3
1 52191U 22033AL 24146.50949412 .15429445 25297-5 22962-3 0 9997
2 52191 97.2978 240.3180 0016695 271.5522 88.3869 16.47492065120493Epoch: 2024-05-25T12:13Z
TLE epoch observation values (Epoch: 2024-05-25T12:13:40.291Z)
Latitude
-0.00008°
Longitude
173.32645°
Altitude
148.924 km
Speed
7.817 km/s
True Right ascension
16h 01m 16s
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
20:38:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
153.628 km
Perigee altitude
131.855 km
Semi-major axis
6,520.878 km
Eccentricity
0.00167
Inclination
97.2978°
RAAN
240.318°
Arg. of periapsis
271.5522°
True anomaly
88.57815°
Mean anomaly
88.3869°
Eccentric anomaly
88.48252°
Mean motion
4.12177 °/min
Orbital period
87.34 mins
BSTAR
0.00022962
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Other satellites on launch #33 in the year 2022 (2022-04-01 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.SUCHAI-3 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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