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 25198.75050048 .00001530 00000-0 13846-3 0 9991
2 60235 61.9946 312.6431 0059907 59.3215 301.3759 14.98887968 55835
| Epoch (UTC): | 17 July 2025 18:00:43 |
| Eccentricity: | 0.0059907 |
| inclination: | 61.9946° |
| perigee height: | 529 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 312.6431° |
| argument of perigee: | 59.3215° |
| revolutions per day: | 14.98887968 |
| mean anomaly at epoch: | 301.3759° |
| orbit number at epoch: | 5583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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