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 26280U 99057FS 24357.69280646 .00000813 00000-0 27371-3 0 9995
2 26280 98.7950 26.1924 0085520 356.1667 122.4875 14.37834115296638
| Epoch (UTC): | 22 December 2024 16:37:38 |
| Eccentricity: | 0.0085520 |
| inclination: | 98.7950° |
| perigee height: | 704 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 26.1924° |
| argument of perigee: | 356.1667° |
| revolutions per day: | 14.37834115 |
| mean anomaly at epoch: | 122.4875° |
| orbit number at epoch: | 29663 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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