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 25197.61640293 .00001544 00000-0 13957-3 0 9990
2 60235 61.9946 316.5739 0059807 59.0614 301.6334 14.98883609 55669
| Epoch (UTC): | 16 July 2025 14:47:37 |
| Eccentricity: | 0.0059807 |
| inclination: | 61.9946° |
| perigee height: | 529 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 316.5739° |
| argument of perigee: | 59.0614° |
| revolutions per day: | 14.98883609 |
| mean anomaly at epoch: | 301.6334° |
| orbit number at epoch: | 5566 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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