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 24250.58101355 .00007490 00000-0 68682-3 0 9997
2 60235 61.9975 319.1836 0018932 304.9803 54.9506 14.95522773 8783
| Epoch (UTC): | 06 September 2024 13:56:39 |
| Eccentricity: | 0.0018932 |
| inclination: | 61.9975° |
| perigee height: | 567 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 319.1836° |
| argument of perigee: | 304.9803° |
| revolutions per day: | 14.95522773 |
| mean anomaly at epoch: | 54.9506° |
| orbit number at epoch: | 878 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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