STARLINK-32917, 62921
Orbit data source: Space-Track
STARLINK-32917, 62921 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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62921 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-32917
1 62921U 25027Q 25255.72060871 .00024840 00000-0 90948-3 0 9997
2 62921 42.9981 53.9910 0000864 251.9905 108.0853 15.27568325 34322
TLE epoch observation values (Epoch: 2025-09-12T17:17:40.592Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #27 in the year 2025 (2025-02-08 UTC)
STARLINK-32917 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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4 mins | 2025-09-13 20:30:36.439Z | 252.396° W | 2025-09-13 20:32:36.439Z | 219.772° SW | 14.117° | 2025-09-13 20:34:36.439Z | 186.237° SSW |
5 mins | 2025-09-14 13:27:36.439Z | 203.655° SW | 2025-09-14 13:29:36.439Z | 138.848° SSE | 31.641° | 2025-09-14 13:32:36.439Z | 82.89° E |
6 mins | 2025-09-14 15:05:36.439Z | 267.791° W | 2025-09-14 15:08:36.439Z | 29.034° NE | 40.691° | 2025-09-14 15:11:36.439Z | 70.22° E |
5 mins | 2025-09-14 16:45:36.439Z | 299.183° NW | 2025-09-14 16:47:36.439Z | 21.457° NNE | 38.59° | 2025-09-14 16:50:36.439Z | 82.606° E |
5 mins | 2025-09-14 18:24:36.439Z | 278.294° WNW | 2025-09-14 18:26:36.439Z | 181.334° SSW | 42.26° | 2025-09-14 18:29:36.439Z | 121.706° SE |
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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