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 36326U 82025L 24354.30126598 .00008159 00000-0 37955-2 0 9993
2 36326 82.5170 355.5061 0027330 91.1344 269.2968 14.20259035 26569
| Epoch (UTC): | 19 December 2024 07:13:49 |
| Eccentricity: | 0.0027330 |
| inclination: | 82.5170° |
| perigee height: | 805 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 355.5061° |
| argument of perigee: | 91.1344° |
| revolutions per day: | 14.20259035 |
| mean anomaly at epoch: | 269.2968° |
| orbit number at epoch: | 2656 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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