STARLINK-1185, 45087
Orbit data source: Space-Track
STARLINK-1185, 45087 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 29 Jan 2020 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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45087 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-1185
1 45087U 20006AV 25286.05543918 -.00002415 00000-0 -14330-3 0 9998
2 45087 53.0533 189.3733 0001447 78.5431 281.5721 15.06390507314777
TLE epoch observation values (Epoch: 2025-10-13T01:19:49.945Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #6 in the year 2020 (2020-01-29 UTC)
STARLINK-1185 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 | 2025-10-14 18:52:29.014Z | 176.508° S | 2025-10-14 18:55:29.014Z | 127.423° SE | 19.724° | 2025-10-14 18:58:29.014Z | 79.399° E |
6 mins | 2025-10-14 20:32:29.014Z | 255.889° W | 2025-10-14 20:34:29.014Z | 312.417° NW | 38.855° | 2025-10-14 20:38:29.014Z | 42.365° NE |
4 mins | 2025-10-14 22:13:29.014Z | 319.081° NNW | 2025-10-14 22:14:29.014Z | 336.006° NNW | 15.951° | 2025-10-14 22:17:29.014Z | 24.038° NE |
5 mins | 2025-10-15 01:34:29.014Z | 343.446° N | 2025-10-15 01:36:29.014Z | 27.847° NE | 25.073° | 2025-10-15 01:39:29.014Z | 83.077° E |
6 mins | 2025-10-15 03:13:29.014Z | 295.483° NW | 2025-10-15 03:16:29.014Z | 205.23° SW | 37.938° | 2025-10-15 03:19:29.014Z | 150.437° 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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