DECAYED
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TRSI-3, 52418 (Decayed)

Orbit data source: Space-Track

TRSI-3, 52418 was an American payload satellite in LEO that was launched on Mon, 02 May 2022 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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
52418, 2022-047AA
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
TRSI/ACMEO
Mission
Decayed Commercial Technology
Bus & Motor
POCKETQUBE 1P, Unknown motor
Mass
0.25 kg wet, 0.25 kg dry
Launch date (UTC)
2022-05-02 (3 years ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.0 m
Radar Cross Section
0.004 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 year ago

TLE from 1 year ago
0 TRSI-3
1 52418U 22047AA  24158.97405842  .05764336  24649-5  14831-2 0  9997
2 52418  97.3666 253.7119 0016439 270.7857  89.1552 16.28371298118564
Epoch: 2024-06-06T23:22Z
TLE epoch observation values (Epoch: 2024-06-06T23:22:38.647Z)
Latitude
-0.0001°
Longitude
7.19154°
Altitude
200.016 km
Speed
7.786 km/s
True Right ascension
16h 54m 50s
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
13:19:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
204.545 km
Perigee altitude
182.938 km
Semi-major axis
6,571.879 km
Eccentricity
0.00164
Inclination
97.3666°
RAAN
253.7119°
Arg. of periapsis
270.7857°
True anomaly
89.34356°
Mean anomaly
89.1552°
Eccentric anomaly
89.24938°
Mean motion
4.07389 °/min
Orbital period
88.37 mins
BSTAR
0.0014831
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