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 19223U 88052A 23272.53155096 .00000079 00000-0 16574-3 0 9992
2 19223 89.9747 79.7507 0032409 73.7280 351.0847 13.22799271703026
| Epoch (UTC): | 29 September 2023 12:45:26 |
| Eccentricity: | 0.0032409 |
| inclination: | 89.9747° |
| perigee height: | 1149 km |
| apogee height: | 1198 km |
| right ascension of ascending node: | 79.7507° |
| argument of perigee: | 73.7280° |
| revolutions per day: | 13.22799271 |
| mean anomaly at epoch: | 351.0847° |
| orbit number at epoch: | 70302 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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