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 57418C 23102Q 24358.47756944 .00009208 00000+0 67944-3 0 3581
2 57418 43.0015 125.9870 0001515 264.0955 333.8011 15.02525018 14
| Epoch (UTC): | 23 December 2024 11:27:42 |
| Eccentricity: | 0.0001515 |
| inclination: | 43.0015° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 125.9870° |
| argument of perigee: | 264.0955° |
| revolutions per day: | 15.02525018 |
| mean anomaly at epoch: | 333.8011° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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