STARLINK-1067, 44771
Orbit data source: Space-Track
STARLINK-1067, 44771 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 11 Nov 2019 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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44771 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 STARLINK-1067
1 44771U 19074BL 25287.64963191 .00006975 00000-0 48674-3 0 9996
2 44771 53.0522 162.2197 0002162 86.3045 273.8191 15.06398127326180
TLE epoch observation values (Epoch: 2025-10-14T15:35:28.197Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #74 in the year 2019 (2019-11-11 UTC)
STARLINK-1067 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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6 mins | 2025-10-15 17:12:36.326Z | 177.94° S | 2025-10-15 17:15:36.326Z | 129.993° SE | 19.912° | 2025-10-15 17:18:36.326Z | 80.329° E |
6 mins | 2025-10-15 18:52:36.326Z | 255.322° W | 2025-10-15 18:54:36.326Z | 305.728° NW | 38.292° | 2025-10-15 18:58:36.326Z | 41.788° NE |
4 mins | 2025-10-15 20:33:36.326Z | 317.427° NNW | 2025-10-15 20:35:36.326Z | 352.238° N | 15.875° | 2025-10-15 20:37:36.326Z | 22.697° NE |
5 mins | 2025-10-15 23:54:36.326Z | 341.744° N | 2025-10-15 23:56:36.326Z | 24.89° NE | 25.184° | 2025-10-15 23:59:36.326Z | 82.323° E |
6 mins | 2025-10-16 01:33:36.326Z | 295.829° NW | 2025-10-16 01:36:36.326Z | 211.466° SW | 38.026° | 2025-10-16 01:39:36.326Z | 151.333° 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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