TSAT-1A, 59442
Orbit data source: Space-Track
TSAT-1A, 59442 is a payload satellite owned by TASL (IN) in LEO that was launched on Sun, 07 Apr 2024 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.
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59442 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 TSAT-1A
1 59442U 24066A 25293.59488571 .00018744 00000-0 67063-3 0 9999
2 59442 45.6213 343.7641 0011318 226.7280 133.2670 15.28546954 85022
TLE epoch observation values (Epoch: 2025-10-20T14:16:38.125Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #66 in the year 2024 (2024-04-07 UTC)
TSAT-1A Visibility forecast
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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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5 mins | 2025-10-22 05:40:39.804Z | 193.263° SSW | 2025-10-22 05:42:39.804Z | 151.426° SSE | 24.763° | 2025-10-22 05:45:39.804Z | 87.848° E |
5 mins | 2025-10-22 07:19:39.804Z | 266.091° W | 2025-10-22 07:21:39.804Z | 1.395° NNE | 41.338° | 2025-10-22 07:24:39.804Z | 60.136° ENE |
5 mins | 2025-10-22 08:58:39.804Z | 307.591° NW | 2025-10-22 09:00:39.804Z | 3.011° NNE | 28.732° | 2025-10-22 09:03:39.804Z | 61.952° ENE |
5 mins | 2025-10-22 10:37:39.804Z | 311.262° NW | 2025-10-22 10:39:39.804Z | 16.047° NNE | 36.971° | 2025-10-22 10:42:39.804Z | 89.664° E |
5 mins | 2025-10-22 12:16:39.804Z | 267.749° W | 2025-10-22 12:18:39.804Z | 197.6° SSW | 32.965° | 2025-10-22 12:21:39.804Z | 143.134° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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