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 25348.33264022 .00003613 00000-0 29296-3 0 9991
2 60235 61.9925 153.7398 0064297 93.4909 267.3538 15.00038160 78269
| Epoch (UTC): | 14 December 2025 07:59:00 |
| Eccentricity: | 0.0064297 |
| inclination: | 61.9925° |
| perigee height: | 522 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 153.7398° |
| argument of perigee: | 93.4909° |
| revolutions per day: | 15.00038160 |
| mean anomaly at epoch: | 267.3538° |
| orbit number at epoch: | 7826 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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