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 26575U 00065A 21015.91296003 -.00000333 00000-0 00000-0 0 9995
2 26575 8.2406 48.7240 0001827 272.4894 257.4079 1.00267787 13091
| Epoch (UTC): | 15 January 2021 21:54:39 |
| Eccentricity: | 0.0001827 |
| inclination: | 8.2406° |
| perigee height: | 35779 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 48.7240° |
| argument of perigee: | 272.4894° |
| revolutions per day: | 1.00267787 |
| mean anomaly at epoch: | 257.4079° |
| orbit number at epoch: | 1309 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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