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 25194.54765117 .00001586 00000-0 14302-3 0 9993
2 60235 61.9946 327.2102 0059566 58.3592 302.3289 14.98872589 55203
| Epoch (UTC): | 13 July 2025 13:08:37 |
| Eccentricity: | 0.0059566 |
| inclination: | 61.9946° |
| perigee height: | 529 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 327.2102° |
| argument of perigee: | 58.3592° |
| revolutions per day: | 14.98872589 |
| mean anomaly at epoch: | 302.3289° |
| orbit number at epoch: | 5520 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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