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 25341.26649142 .00004376 00000-0 35175-3 0 9996
2 60235 61.9919 178.2760 0064437 91.9659 268.8812 14.99975893 77202
| Epoch (UTC): | 07 December 2025 06:23:44 |
| Eccentricity: | 0.0064437 |
| inclination: | 61.9919° |
| perigee height: | 522 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 178.2760° |
| argument of perigee: | 91.9659° |
| revolutions per day: | 14.99975893 |
| mean anomaly at epoch: | 268.8812° |
| orbit number at epoch: | 7720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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