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 26907U 01040C 24287.13474629 0.00000000 00000-0 00000-0 0 01
2 26907 63.3531 12.5747 0593043 9.6388 350.6308 13.41844203 06
| Epoch (UTC): | 13 October 2024 03:14:02 |
| Eccentricity: | 0.0593043 |
| inclination: | 63.3531° |
| perigee height: | 659 km |
| apogee height: | 1546 km |
| right ascension of ascending node: | 12.5747° |
| argument of perigee: | 9.6388° |
| revolutions per day: | 13.41844203 |
| mean anomaly at epoch: | 350.6308° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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