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 24254.72635169 .00007254 00000-0 66467-3 0 9999
2 60235 61.9969 304.8906 0019340 308.4556 51.4796 14.95584664 9403
| Epoch (UTC): | 10 September 2024 17:25:56 |
| Eccentricity: | 0.0019340 |
| inclination: | 61.9969° |
| perigee height: | 567 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 304.8906° |
| argument of perigee: | 308.4556° |
| revolutions per day: | 14.95584664 |
| mean anomaly at epoch: | 51.4796° |
| orbit number at epoch: | 940 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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