DECAYED
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SUCHAI-2, 52192 (Decayed)

Orbit data source: Space-Track

SUCHAI-2, 52192 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.

Not visible in the next 10 days
Identifier
52192, 2022-033AM
Orbit
Decayed
Country
Flag of UnknownUnknown / CHLE
Related business
Flag of CLSpace 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)
2022-04-01 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 11 months ago

TLE from 11 months ago
0 SUCHAI-2
1 52192U 22033AM  24280.41582610  .16355900  25290-5  20957-3 0  9990
2 52192  97.2596  13.1096 0010468 260.4666  99.5456 16.49110273141185
Epoch: 2024-10-06T09:58Z
TLE epoch observation values (Epoch: 2024-10-06T09:58:47.375Z)
Latitude
0.00002°
Longitude
-152.1459°
Altitude
146.086 km
Speed
7.818 km/s
True Right ascension
00h 52m 26s
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
20:40:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
145.291 km
Perigee altitude
131.647 km
Semi-major axis
6,516.606 km
Eccentricity
0.00105
Inclination
97.2596°
RAAN
13.1096°
Arg. of periapsis
260.4666°
True anomaly
99.66387°
Mean anomaly
99.5456°
Eccentric anomaly
99.60474°
Mean motion
4.12583 °/min
Orbital period
87.26 mins
BSTAR
0.00020957
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