CYGFM02, 41886
Orbit data source: Space-Track
CYGFM02, 41886 is an American payload satellite in LEO that was launched on Thu, 15 Dec 2016 UTC via a PEGASUS XL launch vehicle from the Pegasus Launch, Eastern Range Air Space (ERAS). 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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41886 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CYGFM02
1 41886U 16078C 25256.33707824 .00013209 00000-0 26111-3 0 9992
2 41886 34.9438 252.1122 0008203 85.1251 275.0407 15.46207796486044
TLE epoch observation values (Epoch: 2025-09-13T08:05:23.559Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #78 in the year 2016 (2016-12-15 UTC)
CYGFM02 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 | 2025-09-15 03:44:37.164Z | 217.582° SW | 2025-09-15 03:46:37.164Z | 179.421° S | 21.138° | 2025-09-15 03:49:37.164Z | 113.077° SE |
4 mins | 2025-09-15 05:23:37.164Z | 225.645° WSW | 2025-09-15 05:24:37.164Z | 194.903° SSW | 28.716° | 2025-09-15 05:27:37.164Z | 117.201° 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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