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.
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52420 intel report (Beta)
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TRSI-2 radio frequencies
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TRSI-2 details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 5 months ago |
| Origin | |
| 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) | |
| Launch vehicle | |
| Launch site | |
| 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 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 16.37177951117524Epoch: 2024-05-31T04:48Z
Definitive object data (Epoch: 2024-05-31T04:48:16.809Z)
| Latitude | -0.00009° |
| Longitude | -74.34853° |
| Altitude | 176.047 km |
| Speed | 7.801 km/s |
| True Right ascension | 16h 27m 37s |
| 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 | 180.547 km |
| Perigee | 159.712 km |
| Semi-major axis | 6,548.267 km |
| Eccentricity | 0.0015909 |
| Inclination | 97.3608° |
| RAAN | 246.9042° |
| Arg. of periapsis | 272.9087° |
| True anomaly | 87.22108° |
| Mean anomaly | 87.039° |
| Eccentric anomaly | 87.13004° |
| Mean motion | 4.09594 °/min |
| BSTAR | 0.001132 |
| Period | 87.89 mins |
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Other satellites on launch #47 in the year 2022 (2022-05-02 UTC)
TRSI-2 Visibility forecast
Observer location: undefined°, undefined
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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