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 25189.54420247 .00001610 00000-0 14506-3 0 9993
2 60235 61.9954 344.5519 0059185 57.1409 303.5357 14.98854351 54459
| Epoch (UTC): | 08 July 2025 13:03:39 |
| Eccentricity: | 0.0059185 |
| inclination: | 61.9954° |
| perigee height: | 529 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 344.5519° |
| argument of perigee: | 57.1409° |
| revolutions per day: | 14.98854351 |
| mean anomaly at epoch: | 303.5357° |
| orbit number at epoch: | 5445 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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