STARLINK-1695, 46329
Orbit data source: Space-Track
STARLINK-1695, 46329 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 03 Sep 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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46329 intel report (Beta)
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TLE from 8 hours ago
0 STARLINK-1695
1 46329U 20062E 25199.61370647 -.00000049 00000-0 15583-4 0 9994
2 46329 53.0557 327.4257 0001209 98.7587 261.3539 15.06397417269488
TLE epoch observation values (Epoch: 2025-07-18T14:43:44.239Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #62 in the year 2020 (2020-09-03 UTC)
STARLINK-1695 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 | 2025-07-19 09:59:28.855Z | 162.423° S | 2025-07-19 10:01:28.855Z | 128.631° SE | 17.351° | 2025-07-19 10:03:28.855Z | 94.018° ESE |
6 mins | 2025-07-19 11:38:28.855Z | 249.239° W | 2025-07-19 11:40:28.855Z | 304.387° NW | 41.04° | 2025-07-19 11:44:28.855Z | 44.09° NE |
4 mins | 2025-07-19 13:19:28.855Z | 317.313° NNW | 2025-07-19 13:20:28.855Z | 334.818° NNW | 16.77° | 2025-07-19 13:23:28.855Z | 23.855° NE |
5 mins | 2025-07-19 16:40:28.855Z | 344.262° N | 2025-07-19 16:42:28.855Z | 26.491° NE | 23.429° | 2025-07-19 16:45:28.855Z | 79.647° E |
6 mins | 2025-07-19 18:19:28.855Z | 299.695° NW | 2025-07-19 18:22:28.855Z | 202.367° SSW | 40.898° | 2025-07-19 18:25:28.855Z | 145.355° 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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