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 25349.19922406 .00002472 00000-0 20584-3 0 9996
2 60235 61.9925 150.7305 0064300 93.6908 267.1538 15.00040885 78399
| Epoch (UTC): | 15 December 2025 04:46:52 |
| Eccentricity: | 0.0064300 |
| inclination: | 61.9925° |
| perigee height: | 522 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 150.7305° |
| argument of perigee: | 93.6908° |
| revolutions per day: | 15.00040885 |
| mean anomaly at epoch: | 267.1538° |
| orbit number at epoch: | 7839 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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