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 22181.49440968 .00015762 00000-0 29603-3 0 9998
2 45117 51.6372 349.9735 0008390 218.8732 141.1654 15.48742910135456
| Epoch (UTC): | 30 June 2022 11:51:56 |
| Eccentricity: | 0.0008390 |
| inclination: | 51.6372° |
| perigee height: | 415 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 349.9735° |
| argument of perigee: | 218.8732° |
| revolutions per day: | 15.48742910 |
| mean anomaly at epoch: | 141.1654° |
| orbit number at epoch: | 13545 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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