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 21808U 91076D 23080.77477223 0.00007000 00000-0 85841-3 0 03
2 21808 63.3260 44.8440 0896862 53.7123 306.2877 13.43968536 06
| Epoch (UTC): | 21 March 2023 18:35:40 |
| Eccentricity: | 0.0896862 |
| inclination: | 63.3260° |
| perigee height: | 424 km |
| apogee height: | 1765 km |
| right ascension of ascending node: | 44.8440° |
| argument of perigee: | 53.7123° |
| revolutions per day: | 13.43968536 |
| mean anomaly at epoch: | 306.2877° |
| 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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