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 22141.84721914 .00046491 00000-0 92380-3 0 9991
2 45117 51.6363 185.7079 0009277 61.6607 298.5315 15.46459280129315
| Epoch (UTC): | 21 May 2022 20:19:59 |
| Eccentricity: | 0.0009277 |
| inclination: | 51.6363° |
| perigee height: | 421 km |
| apogee height: | 433 km |
| right ascension of ascending node: | 185.7079° |
| argument of perigee: | 61.6607° |
| revolutions per day: | 15.46459280 |
| mean anomaly at epoch: | 298.5315° |
| orbit number at epoch: | 12931 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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