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 61365U 24140WE 24357.41161123 .00003639 00000-0 51108-3 0 9991
2 61365 89.1364 336.8091 0172805 276.8683 81.2901 14.67424474 16019
| Epoch (UTC): | 22 December 2024 09:52:43 |
| Eccentricity: | 0.0172805 |
| inclination: | 89.1364° |
| perigee height: | 547 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 336.8091° |
| argument of perigee: | 276.8683° |
| revolutions per day: | 14.67424474 |
| mean anomaly at epoch: | 81.2901° |
| orbit number at epoch: | 1601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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