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 9510U 76108B 24357.94299164 .00000179 00000-0 16275-3 0 9993
2 9510 82.9366 140.5859 0026939 53.3154 307.0473 13.77808556419810
| Epoch (UTC): | 22 December 2024 22:37:54 |
| Eccentricity: | 0.0026939 |
| inclination: | 82.9366° |
| perigee height: | 952 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 140.5859° |
| argument of perigee: | 53.3154° |
| revolutions per day: | 13.77808556 |
| mean anomaly at epoch: | 307.0473° |
| orbit number at epoch: | 41981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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