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 60235U 24128A 25188.61021883 .00001780 00000-0 15853-3 0 9997
2 60235 61.9953 347.7891 0059097 56.9295 303.7449 14.98850668 54314
| Epoch (UTC): | 07 July 2025 14:38:42 |
| Eccentricity: | 0.0059097 |
| inclination: | 61.9953° |
| perigee height: | 529 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 347.7891° |
| argument of perigee: | 56.9295° |
| revolutions per day: | 14.98850668 |
| mean anomaly at epoch: | 303.7449° |
| orbit number at epoch: | 5431 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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