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 17191U 86097A 24357.63260105 .00015833 00000-0 50632-3 0 9992
2 17191 82.4665 190.4023 0003304 324.5290 35.5731 15.32303312 79100
| Epoch (UTC): | 22 December 2024 15:10:56 |
| Eccentricity: | 0.0003304 |
| inclination: | 82.4665° |
| perigee height: | 466 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 190.4023° |
| argument of perigee: | 324.5290° |
| revolutions per day: | 15.32303312 |
| mean anomaly at epoch: | 35.5731° |
| orbit number at epoch: | 7910 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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