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 54515U 22151JT 24280.79368641 .00002468 00000-0 78172-3 0 9999
2 54515 98.6054 295.1819 0120451 41.9301 319.1031 14.36918278 99476
| Epoch (UTC): | 06 October 2024 19:02:54 |
| Eccentricity: | 0.0120451 |
| inclination: | 98.6054° |
| perigee height: | 682 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 295.1819° |
| argument of perigee: | 41.9301° |
| revolutions per day: | 14.36918278 |
| mean anomaly at epoch: | 319.1031° |
| orbit number at epoch: | 9947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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