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 25342.26643647 .00004108 00000-0 33118-3 0 9999
2 60235 61.9920 174.8039 0064426 92.1881 268.6588 14.99983475 77352
| Epoch (UTC): | 08 December 2025 06:23:40 |
| Eccentricity: | 0.0064426 |
| inclination: | 61.9920° |
| perigee height: | 522 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 174.8039° |
| argument of perigee: | 92.1881° |
| revolutions per day: | 14.99983475 |
| mean anomaly at epoch: | 268.6588° |
| orbit number at epoch: | 7735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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