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 21809U 91076E 23086.82358746 0.00008000 00000-0 91904-3 0 02
2 21809 63.3075 25.4749 0904883 51.3853 308.6147 13.44188410 07
| Epoch (UTC): | 27 March 2023 19:45:57 |
| Eccentricity: | 0.0904883 |
| inclination: | 63.3075° |
| perigee height: | 417 km |
| apogee height: | 1770 km |
| right ascension of ascending node: | 25.4749° |
| argument of perigee: | 51.3853° |
| revolutions per day: | 13.44188410 |
| mean anomaly at epoch: | 308.6147° |
| 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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