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 35605U 93036AMY 24355.71508672 .00039831 00000-0 50515-2 0 9997
2 35605 73.8890 350.3268 0065952 351.6004 8.4061 14.79979154606152
| Epoch (UTC): | 20 December 2024 17:09:43 |
| Eccentricity: | 0.0065952 |
| inclination: | 73.8890° |
| perigee height: | 583 km |
| apogee height: | 675 km |
| right ascension of ascending node: | 350.3268° |
| argument of perigee: | 351.6004° |
| revolutions per day: | 14.79979154 |
| mean anomaly at epoch: | 8.4061° |
| orbit number at epoch: | 60615 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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