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). Payloads include a variety of satellites, spacecraft, and rockets 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
Last TLE update	9 months ago
Origin	ACMEO/TRSI (US)
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, 0.05 m
Radar Cross Section	0.004 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 9 months 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

Definitive object data (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 TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	204.545 km
Perigee altitude	182.938 km
Semi-major axis	6,571.879 km
Eccentricity	0.0016439
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
BSTAR	0.0014831
Orbital period	88.37 mins