STARLINK-1080, 44961
Orbit data source: Space-Track
STARLINK-1080, 44961 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 07 Jan 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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44961 intel report (Beta)
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TLE from 12 hours ago
0 STARLINK-1080
1 44961U 20001AZ 25199.48563171 .00001177 00000-0 97931-4 0 9997
2 44961 53.0548 278.0071 0001221 93.6372 266.4757 15.06394725305111
TLE epoch observation values (Epoch: 2025-07-18T11:39:18.579Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #1 in the year 2020 (2020-01-07 UTC)
STARLINK-1080 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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6 mins | 2025-07-19 06:54:34.607Z | 180.008° SSW | 2025-07-19 06:57:34.607Z | 128.363° SE | 21.819° | 2025-07-19 07:00:34.607Z | 77.767° E |
6 mins | 2025-07-19 08:34:34.607Z | 260.075° W | 2025-07-19 08:36:34.607Z | 311.94° NW | 36.699° | 2025-07-19 08:40:34.607Z | 40.719° NE |
4 mins | 2025-07-19 10:15:34.607Z | 319.076° NNW | 2025-07-19 10:17:34.607Z | 353.187° N | 15.383° | 2025-07-19 10:19:34.607Z | 23.187° NE |
5 mins | 2025-07-19 13:36:34.607Z | 341.323° N | 2025-07-19 13:38:34.607Z | 26.452° NE | 26.522° | 2025-07-19 13:41:34.607Z | 85.228° E |
6 mins | 2025-07-19 15:15:34.607Z | 292.671° NW | 2025-07-19 15:18:34.607Z | 210.845° SW | 35.585° | 2025-07-19 15:21:34.607Z | 154.807° 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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