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 26351U 99057JL 24357.89679113 .00002817 00000-0 70314-3 0 9998
2 26351 98.6397 357.8523 0056239 234.4687 125.1255 14.51464161305915
| Epoch (UTC): | 22 December 2024 21:31:22 |
| Eccentricity: | 0.0056239 |
| inclination: | 98.6397° |
| perigee height: | 681 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 357.8523° |
| argument of perigee: | 234.4687° |
| revolutions per day: | 14.51464161 |
| mean anomaly at epoch: | 125.1255° |
| orbit number at epoch: | 30591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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