View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 22184U 92068C 25347.58782226 .00000039 00000-0 16053-3 0 9993
2 22184 82.5993 105.1856 0003272 175.7086 194.9678 12.62606632527539
| Epoch (UTC): | 13 December 2025 14:06:27 |
| Eccentricity: | 0.0003272 |
| inclination: | 82.5993° |
| perigee height: | 1409 km |
| apogee height: | 1415 km |
| right ascension of ascending node: | 105.1856° |
| argument of perigee: | 175.7086° |
| revolutions per day: | 12.62606632 |
| mean anomaly at epoch: | 194.9678° |
| orbit number at epoch: | 52753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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