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 22267.29898407 .00048395 00000-0 72272-3 0 9994
2 45117 51.6335 283.9870 0005149 154.8812 205.2430 15.54536632148771
| Epoch (UTC): | 24 September 2022 07:10:32 |
| Eccentricity: | 0.0005149 |
| inclination: | 51.6335° |
| perigee height: | 400 km |
| apogee height: | 407 km |
| right ascension of ascending node: | 283.9870° |
| argument of perigee: | 154.8812° |
| revolutions per day: | 15.54536632 |
| mean anomaly at epoch: | 205.2430° |
| orbit number at epoch: | 14877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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