STARLINK-33984, 63830
Orbit data source: Space-Track
STARLINK-33984, 63830 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 04 May 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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63830 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-33984
1 63830U 25092AC 25255.69464305 .00019779 00000-0 72615-3 0 9991
2 63830 43.0012 97.6640 0001809 270.6685 89.3959 15.27588121 21394
TLE epoch observation values (Epoch: 2025-09-12T16:40:17.159Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #92 in the year 2025 (2025-05-04 UTC)
STARLINK-33984 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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5 mins | 2025-09-13 22:59:56.142Z | 264.19° W | 2025-09-13 23:02:56.142Z | 210.455° SW | 19.248° | 2025-09-13 23:04:56.142Z | 173.132° S |
4 mins | 2025-09-14 15:57:56.142Z | 184.053° SSW | 2025-09-14 15:58:56.142Z | 158.773° S | 24.926° | 2025-09-14 16:01:56.142Z | 92.867° ESE |
5 mins | 2025-09-14 17:35:56.142Z | 259.548° W | 2025-09-14 17:37:56.142Z | 321.721° NNW | 44.342° | 2025-09-14 17:40:56.142Z | 70.051° E |
5 mins | 2025-09-14 19:14:56.142Z | 292.065° WNW | 2025-09-14 19:16:56.142Z | 344.838° N | 37.588° | 2025-09-14 19:19:56.142Z | 74.972° E |
6 mins | 2025-09-14 20:53:56.142Z | 287.186° WNW | 2025-09-14 20:55:56.142Z | 277.764° WNW | 43.339° | 2025-09-14 20:59:56.142Z | 111.225° ESE |
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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