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 04588U 70086A 24357.81086716 .00000375 00000-0 13618-3 0 9991
2 04588 74.0551 128.4744 0012833 24.0889 89.5588 14.36673371835164
| Epoch (UTC): | 22 December 2024 19:27:38 |
| Eccentricity: | 0.0012833 |
| inclination: | 74.0551° |
| perigee height: | 760 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 128.4744° |
| argument of perigee: | 24.0889° |
| revolutions per day: | 14.36673371 |
| mean anomaly at epoch: | 89.5588° |
| orbit number at epoch: | 83516 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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