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 17242U 86101B 23027.54141705 .00000043 00000-0 25485-4 0 9998
2 17242 82.5305 193.2894 0016158 66.5732 357.5450 13.83314068822926
| Epoch (UTC): | 27 January 2023 12:59:38 |
| Eccentricity: | 0.0016158 |
| inclination: | 82.5305° |
| perigee height: | 940 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 193.2894° |
| argument of perigee: | 66.5732° |
| revolutions per day: | 13.83314068 |
| mean anomaly at epoch: | 357.5450° |
| orbit number at epoch: | 82292 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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