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 25344.59962006 .00004373 00000-0 35131-3 0 9991
2 60235 61.9923 166.7024 0064372 92.7020 268.1440 15.00003123 77707
| Epoch (UTC): | 10 December 2025 14:23:27 |
| Eccentricity: | 0.0064372 |
| inclination: | 61.9923° |
| perigee height: | 522 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 166.7024° |
| argument of perigee: | 92.7020° |
| revolutions per day: | 15.00003123 |
| mean anomaly at epoch: | 268.1440° |
| orbit number at epoch: | 7770 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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