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 17160U 86093B 22224.79824772 .00000045 00000-0 31767-4 0 9996
2 17160 82.9269 107.6572 0037823 303.3405 124.4970 13.74672426791244
| Epoch (UTC): | 12 August 2022 19:09:28 |
| Eccentricity: | 0.0037823 |
| inclination: | 82.9269° |
| perigee height: | 955 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 107.6572° |
| argument of perigee: | 303.3405° |
| revolutions per day: | 13.74672426 |
| mean anomaly at epoch: | 124.4970° |
| orbit number at epoch: | 79124 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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