LEGION 6, 62901
Orbit data source: Space-Track
LEGION 6, 62901 is a payload satellite owned by Maxar Intel (US) in LEO that was launched on Tue, 04 Feb 2025 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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62901 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 LEGION 6
1 62901U 25025B 25259.33034385 .00005423 00000-0 30471-3 0 9996
2 62901 44.9931 238.3614 0018023 13.5793 346.5567 15.14233496 34088
TLE epoch observation values (Epoch: 2025-09-16T07:55:41.708Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #25 in the year 2025 (2025-02-04 UTC)
LEGION 6 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 06:31:23.082Z | 297.576° NW | 2025-09-17 06:34:23.082Z | 350.809° N | 41.993° | 2025-09-17 06:38:23.082Z | 102.525° ESE |
5 mins | 2025-09-17 08:12:23.082Z | 259.36° W | 2025-09-17 08:14:23.082Z | 209.561° SW | 26.518° | 2025-09-17 08:17:23.082Z | 156.335° SSE |
5 mins | 2025-09-18 01:18:23.082Z | 203.403° SW | 2025-09-18 01:20:23.082Z | 145.108° SSE | 33.057° | 2025-09-18 01:23:23.082Z | 80.504° E |
6 mins | 2025-09-18 02:57:23.082Z | 271.025° WNW | 2025-09-18 03:00:23.082Z | 10.792° NNE | 38.108° | 2025-09-18 03:03:23.082Z | 61.415° ENE |
5 mins | 2025-09-18 04:38:23.082Z | 311.862° NW | 2025-09-18 04:40:23.082Z | 14.513° NNE | 31.732° | 2025-09-18 04:43:23.082Z | 70.633° E |
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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