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 25166.86104609 .00002616 00000-0 22590-3 0 9993
2 60235 61.9949 63.1654 0057181 51.7163 308.9049 14.98759386 51050
| Epoch (UTC): | 15 June 2025 20:39:54 |
| Eccentricity: | 0.0057181 |
| inclination: | 61.9949° |
| perigee height: | 531 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 63.1654° |
| argument of perigee: | 51.7163° |
| revolutions per day: | 14.98759386 |
| mean anomaly at epoch: | 308.9049° |
| orbit number at epoch: | 5105 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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