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: 19 hours ago
TLE from 19 hours ago
0 LEGION 6
1 62901U 25025B 25294.02306032 .00009239 00000-0 49845-3 0 9996
2 62901 44.9956 52.6857 0017879 217.1508 142.8133 15.14969726 39347
TLE epoch observation values (Epoch: 2025-10-21T00:33:12.411Z)
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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5 mins | 2025-10-22 09:57:21.440Z | 182.841° SSW | 2025-10-22 10:00:21.440Z | 131.512° SE | 18.005° | 2025-10-22 10:02:21.440Z | 99.043° ESE |
6 mins | 2025-10-22 11:36:21.440Z | 244.046° WSW | 2025-10-22 11:39:21.440Z | 84.208° E | 44.771° | 2025-10-22 11:42:21.440Z | 66.912° ENE |
6 mins | 2025-10-22 13:16:21.440Z | 288.587° WNW | 2025-10-22 13:19:21.440Z | 3.399° NNE | 33.122° | 2025-10-22 13:22:21.440Z | 62.013° ENE |
5 mins | 2025-10-22 14:57:21.440Z | 311.208° NW | 2025-10-22 14:59:21.440Z | 18.249° NNE | 36.618° | 2025-10-22 15:02:21.440Z | 84.503° E |
6 mins | 2025-10-22 16:36:21.440Z | 282.39° WNW | 2025-10-22 16:39:21.440Z | 184.86° SSW | 38.461° | 2025-10-22 16:42:21.440Z | 133.701° SE |
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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