LEGION 5, 62900
Orbit data source: Space-Track
LEGION 5, 62900 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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62900 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEGION 5
1 62900U 25025A 25260.24348443 .00005255 00000-0 26867-3 0 9997
2 62900 45.0469 324.3699 0016393 270.4548 89.4454 15.17680489 33071
TLE epoch observation values (Epoch: 2025-09-17T05:50:37.054Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #25 in the year 2025 (2025-02-04 UTC)
LEGION 5 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 | 2025-09-18 07:18:39.065Z | 218.711° SW | 2025-09-18 07:21:39.065Z | 166.794° S | 34.191° | 2025-09-18 07:25:39.065Z | 76.118° E |
6 mins | 2025-09-18 08:58:39.065Z | 271.586° WNW | 2025-09-18 09:01:39.065Z | 353.948° N | 38.399° | 2025-09-18 09:04:39.065Z | 59.735° ENE |
5 mins | 2025-09-18 10:39:39.065Z | 311.719° NW | 2025-09-18 10:41:39.065Z | 12.701° NNE | 31.995° | 2025-09-18 10:44:39.065Z | 70.91° E |
6 mins | 2025-09-18 12:18:39.065Z | 297.274° NW | 2025-09-18 12:21:39.065Z | 80.84° E | 42.711° | 2025-09-18 12:24:39.065Z | 108.351° ESE |
4 mins | 2025-09-18 13:58:39.065Z | 255.361° W | 2025-09-18 14:00:39.065Z | 212.074° SW | 22.031° | 2025-09-18 14:02:39.065Z | 173.787° S |
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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