STARLINK-32434, 61913
Orbit data source: Space-Track
STARLINK-32434, 61913 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 11 Nov 2024 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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61913 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-32434
1 61913U 24207B 25261.16846279 .00023325 00000-0 85391-3 0 9998
2 61913 43.0005 176.3632 0001426 275.8968 84.1721 15.27600972 48330
TLE epoch observation values (Epoch: 2025-09-18T04:02:35.185Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #207 in the year 2024 (2024-11-11 UTC)
STARLINK-32434 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 | 2025-09-19 21:02:20.520Z | 207.912° SW | 2025-09-19 21:05:20.520Z | 144.092° SSE | 27.009° | 2025-09-19 21:08:20.520Z | 87.177° E |
6 mins | 2025-09-19 22:41:20.520Z | 260.882° W | 2025-09-19 22:44:20.520Z | 36.054° NE | 42.521° | 2025-09-19 22:47:20.520Z | 70.433° E |
5 mins | 2025-09-20 00:21:20.520Z | 297.516° NW | 2025-09-20 00:23:20.520Z | 15.526° NNE | 37.964° | 2025-09-20 00:26:20.520Z | 78.67° E |
5 mins | 2025-09-20 02:00:20.520Z | 284.817° WNW | 2025-09-20 02:02:20.520Z | 172.328° S | 44.535° | 2025-09-20 02:05:20.520Z | 114.121° SE |
4 mins | 2025-09-20 03:39:20.520Z | 245.906° WSW | 2025-09-20 03:40:20.520Z | 226.455° WSW | 17.906° | 2025-09-20 03:43:20.520Z | 171.168° S |
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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