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 59588U 24077B 24282.74803729 .00013394 00000-0 15047-1 0 9991
2 59588 97.4454 324.6586 0049923 181.4257 178.6761 13.70322541 22939
| Epoch (UTC): | 08 October 2024 17:57:10 |
| Eccentricity: | 0.0049923 |
| inclination: | 97.4454° |
| perigee height: | 961 km |
| apogee height: | 1035 km |
| right ascension of ascending node: | 324.6586° |
| argument of perigee: | 181.4257° |
| revolutions per day: | 13.70322541 |
| mean anomaly at epoch: | 178.6761° |
| orbit number at epoch: | 2293 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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