STRIX-4, 60352
Orbit data source: Space-Track
STRIX-4, 60352 is a payload satellite owned by Synspective (JP) in LEO that was launched on Fri, 02 Aug 2024 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.
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60352 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 STRIX-4
1 60352U 24137A 25260.32413487 .00011974 00000-0 52858-3 0 9993
2 60352 43.0216 25.1195 0016202 312.0052 47.9418 15.21611956 62290
TLE epoch observation values (Epoch: 2025-09-17T07:46:45.252Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #137 in the year 2024 (2024-08-02 UTC)
STRIX-4 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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7 mins | 2025-09-17 16:03:13.051Z | 289.024° WNW | 2025-09-17 16:07:13.051Z | 37.208° NE | 43.475° | 2025-09-17 16:10:13.051Z | 98.507° ESE |
5 mins | 2025-09-17 17:44:13.051Z | 262.737° W | 2025-09-17 17:46:13.051Z | 212.966° SW | 29.245° | 2025-09-17 17:49:13.051Z | 149.627° SSE |
6 mins | 2025-09-18 12:23:13.051Z | 245.136° WSW | 2025-09-18 12:26:13.051Z | 111.445° ESE | 44.161° | 2025-09-18 12:29:13.051Z | 73.287° E |
6 mins | 2025-09-18 14:03:13.051Z | 286.971° WNW | 2025-09-18 14:05:13.051Z | 337.512° N | 38.01° | 2025-09-18 14:09:13.051Z | 74.901° E |
5 mins | 2025-09-18 15:43:13.051Z | 293.952° NW | 2025-09-18 15:45:13.051Z | 31.021° NE | 43.951° | 2025-09-18 15:48:13.051Z | 99.982° ESE |
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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