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 24286.69025005 .00004010 00000-0 44972-2 0 9997
2 59588 97.4516 327.7171 0049146 179.8778 180.2395 13.70813580 23478
| Epoch (UTC): | 12 October 2024 16:33:57 |
| Eccentricity: | 0.0049146 |
| inclination: | 97.4516° |
| perigee height: | 960 km |
| apogee height: | 1033 km |
| right ascension of ascending node: | 327.7171° |
| argument of perigee: | 179.8778° |
| revolutions per day: | 13.70813580 |
| mean anomaly at epoch: | 180.2395° |
| orbit number at epoch: | 2347 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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