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 11321U 79028B 24357.93461174 .00000096 00000-0 82180-4 0 9998
2 11321 82.9227 137.5654 0020016 110.6559 7.0290 13.76730117295502
| Epoch (UTC): | 22 December 2024 22:25:50 |
| Eccentricity: | 0.0020016 |
| inclination: | 82.9227° |
| perigee height: | 961 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 137.5654° |
| argument of perigee: | 110.6559° |
| revolutions per day: | 13.76730117 |
| mean anomaly at epoch: | 7.0290° |
| orbit number at epoch: | 29550 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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