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 25544U 98067A 24357.81415843 .00061122 00000-0 10662-2 0 9994
2 25544 51.6377 100.8061 0005268 355.1085 147.9826 15.50107458487805
| Epoch (UTC): | 22 December 2024 19:32:23 |
| Eccentricity: | 0.0005268 |
| inclination: | 51.6377° |
| perigee height: | 413 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 100.8061° |
| argument of perigee: | 355.1085° |
| revolutions per day: | 15.50107458 |
| mean anomaly at epoch: | 147.9826° |
| orbit number at epoch: | 48780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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