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 17192U 86097B 24357.68639220 .00000851 00000-0 96241-4 0 9997
2 17192 82.5054 198.3782 0017630 49.7067 18.4133 14.85236055 34729
| Epoch (UTC): | 22 December 2024 16:28:24 |
| Eccentricity: | 0.0017630 |
| inclination: | 82.5054° |
| perigee height: | 600 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 198.3782° |
| argument of perigee: | 49.7067° |
| revolutions per day: | 14.85236055 |
| mean anomaly at epoch: | 18.4133° |
| orbit number at epoch: | 3472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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