STARLINK-32921, 62920
Orbit data source: Space-Track
STARLINK-32921, 62920 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 08 Feb 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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62920 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-32921
1 62920U 25027P 25255.70647634 .00028116 00000-0 10268-2 0 9998
2 62920 43.0021 53.8916 0002077 276.5857 83.4759 15.27596627 34327
TLE epoch observation values (Epoch: 2025-09-12T16:57:19.555Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #27 in the year 2025 (2025-02-08 UTC)
STARLINK-32921 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 20:09:01.851Z | 260.127° W | 2025-09-13 20:11:01.851Z | 225.304° WSW | 18.897° | 2025-09-13 20:14:01.851Z | 168.945° S |
5 mins | 2025-09-14 13:06:01.851Z | 194.858° SSW | 2025-09-14 13:08:01.851Z | 147.144° SSE | 25.429° | 2025-09-14 13:11:01.851Z | 89.234° E |
6 mins | 2025-09-14 14:44:01.851Z | 258.241° W | 2025-09-14 14:47:01.851Z | 36.07° NE | 43.471° | 2025-09-14 14:50:01.851Z | 70.6° E |
5 mins | 2025-09-14 16:24:01.851Z | 296.009° NW | 2025-09-14 16:26:01.851Z | 9.976° NNE | 37.985° | 2025-09-14 16:29:01.851Z | 77.174° E |
5 mins | 2025-09-14 18:03:01.851Z | 286.777° WNW | 2025-09-14 18:05:01.851Z | 193.515° SSW | 44.917° | 2025-09-14 18:08:01.851Z | 111.561° 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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