STARLINK-3189, 51464
Orbit data source: Space-Track
STARLINK-3189, 51464 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 03 Feb 2022 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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51464 intel report (Beta)
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TLE from 9 hours ago
0 STARLINK-3189
1 51464U 22010J 25214.30548854 .00000627 00000-0 57499-4 0 9999
2 51464 53.2168 183.9765 0001166 77.1695 282.9428 15.08841172194157
TLE epoch observation values (Epoch: 2025-08-02T07:19:54.209Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #10 in the year 2022 (2022-02-03 UTC)
STARLINK-3189 Visibility forecast
Observer location: undefined°, undefined°
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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4 mins | 2025-08-02 23:22:54.550Z | 156.96° SSE | 2025-08-02 23:24:54.550Z | 124.816° SE | 14.923° | 2025-08-02 23:26:54.550Z | 93.357° ESE |
6 mins | 2025-08-03 01:00:54.550Z | 239.991° WSW | 2025-08-03 01:03:54.550Z | 342.44° N | 43.003° | 2025-08-03 01:06:54.550Z | 44.36° NE |
4 mins | 2025-08-03 02:41:54.550Z | 309.303° NW | 2025-08-03 02:43:54.550Z | 345.411° N | 17.358° | 2025-08-03 02:45:54.550Z | 18.697° NNE |
5 mins | 2025-08-03 06:02:54.550Z | 344.583° N | 2025-08-03 06:04:54.550Z | 23.71° NE | 21.078° | 2025-08-03 06:07:54.550Z | 74.97° E |
6 mins | 2025-08-03 07:41:54.550Z | 305.099° NW | 2025-08-03 07:44:54.550Z | 179.89° S | 43.305° | 2025-08-03 07:47:54.550Z | 138.204° 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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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