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 25196.94928515 .00001515 00000-0 13732-3 0 9990
2 60235 61.9946 318.8861 0059758 58.9018 301.7916 14.98880946 55568
| Epoch (UTC): | 15 July 2025 22:46:58 |
| Eccentricity: | 0.0059758 |
| inclination: | 61.9946° |
| perigee height: | 529 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 318.8861° |
| argument of perigee: | 58.9018° |
| revolutions per day: | 14.98880946 |
| mean anomaly at epoch: | 301.7916° |
| orbit number at epoch: | 5556 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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