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 59588U 24077B 24252.71607484 .00035260 00000-0 40928-1 0 9997
2 59588 97.4120 301.4786 0033931 231.0616 128.7510 13.68389059 18822
| Epoch (UTC): | 08 September 2024 17:11:08 |
| Eccentricity: | 0.0033931 |
| inclination: | 97.4120° |
| perigee height: | 980 km |
| apogee height: | 1030 km |
| right ascension of ascending node: | 301.4786° |
| argument of perigee: | 231.0616° |
| revolutions per day: | 13.68389059 |
| mean anomaly at epoch: | 128.7510° |
| orbit number at epoch: | 1882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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