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 59108U 24043L 24279.84908833 .00006945 00000-0 66256-3 0 9995
2 59108 97.7792 42.1342 0007634 255.4861 104.5512 14.93620348 32073
| Epoch (UTC): | 05 October 2024 20:22:41 |
| Eccentricity: | 0.0007634 |
| inclination: | 97.7792° |
| perigee height: | 581 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 42.1342° |
| argument of perigee: | 255.4861° |
| revolutions per day: | 14.93620348 |
| mean anomaly at epoch: | 104.5512° |
| orbit number at epoch: | 3207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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