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 25318.86632689 .00004788 00000-0 38502-3 0 9998
2 60235 61.9940 256.0396 0064587 86.8120 274.0356 14.99796554 73841
| Epoch (UTC): | 14 November 2025 20:47:30 |
| Eccentricity: | 0.0064587 |
| inclination: | 61.9940° |
| perigee height: | 522 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 256.0396° |
| argument of perigee: | 86.8120° |
| revolutions per day: | 14.99796554 |
| mean anomaly at epoch: | 274.0356° |
| orbit number at epoch: | 7384 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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