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DECAYED
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TRSI-2, 52420 (Decayed)

Orbit data source: Space-Track

TRSI-2, 52420 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
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TRSI-2 details
Identifier
52420, 2022-047AC
Orbit
Decayed
Last TLE update5 months ago
Origin
Flag of USACMEO/TRSI (US)
ManufacturerTRSI/ACMEO
MissionDecayed Commercial Technology
Bus & MotorPOCKETQUBE 1P, Unknown motor
Mass0.25 kg wet, 0.25 kg dry
Launch date (UTC)
2022-05-02 (2 years ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBRBox, 0.05 m
Radar Cross Section0.004 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 5 months ago
0 TRSI-2
1 52420U 22047AC  24152.20019456  .10643135  25104-5  11320-2 0  9998
2 52420  97.3608 246.9042 0015909 272.9087  87.0390 16.37177951117524
Epoch: 2024-05-31T04:48Z
Definitive object data (Epoch: 2024-05-31T04:48:16.809Z)
Latitude-0.00009°
Longitude-74.34853°
Altitude176.047 km
Speed7.801 km/s
True Right ascension16h 27m 37s
True Declination0° 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
Apogee180.547 km
Perigee159.712 km
Semi-major axis6,548.267 km
Eccentricity0.0015909
Inclination97.3608°
RAAN246.9042°
Arg. of periapsis272.9087°
True anomaly87.22108°
Mean anomaly87.039°
Eccentric anomaly87.13004°
Mean motion4.09594 °/min
BSTAR0.001132
Period87.89 mins
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TRSI-2 Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
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Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
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