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 45117U 19071G 22220.43997105 .00046326 00000-0 78824-3 0 9995
2 45117 51.6347 157.0559 0007932 17.6451 342.4812 15.50911797141491
| Epoch (UTC): | 08 August 2022 10:33:33 |
| Eccentricity: | 0.0007932 |
| inclination: | 51.6347° |
| perigee height: | 408 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 157.0559° |
| argument of perigee: | 17.6451° |
| revolutions per day: | 15.50911797 |
| mean anomaly at epoch: | 342.4812° |
| orbit number at epoch: | 14149 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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