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 22176.26745170 .00025944 00000-0 48542-3 0 9996
2 45117 51.6377 15.8181 0008584 196.9863 163.0839 15.48496321134641
| Epoch (UTC): | 25 June 2022 06:25:07 |
| Eccentricity: | 0.0008584 |
| inclination: | 51.6377° |
| perigee height: | 415 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 15.8181° |
| argument of perigee: | 196.9863° |
| revolutions per day: | 15.48496321 |
| mean anomaly at epoch: | 163.0839° |
| orbit number at epoch: | 13464 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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