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 21805U 91080B 23272.12827071 -.00000148 00000-0 00000-0 0 9992
2 21805 14.5430 352.6808 0006629 113.6166 232.3325 0.99184634 15868
| Epoch (UTC): | 29 September 2023 03:04:42 |
| Eccentricity: | 0.0006629 |
| inclination: | 14.5430° |
| perigee height: | 36065 km |
| apogee height: | 36122 km |
| right ascension of ascending node: | 352.6808° |
| argument of perigee: | 113.6166° |
| revolutions per day: | 0.99184634 |
| mean anomaly at epoch: | 232.3325° |
| orbit number at epoch: | 1586 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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