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 24262.54855170 .00005219 00000-0 48186-3 0 9991
2 60235 61.9950 277.9174 0020125 314.2741 45.6695 14.95689979 10572
| Epoch (UTC): | 18 September 2024 13:09:54 |
| Eccentricity: | 0.0020125 |
| inclination: | 61.9950° |
| perigee height: | 566 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 277.9174° |
| argument of perigee: | 314.2741° |
| revolutions per day: | 14.95689979 |
| mean anomaly at epoch: | 45.6695° |
| orbit number at epoch: | 1057 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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