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 25200.47684205 .00008833 00000-0 84803-2 0 9997
2 59588 97.4449 187.9239 0076220 55.2956 305.5351 13.79047893 61945
| Epoch (UTC): | 19 July 2025 11:26:39 |
| Eccentricity: | 0.0076220 |
| inclination: | 97.4449° |
| perigee height: | 911 km |
| apogee height: | 1023 km |
| right ascension of ascending node: | 187.9239° |
| argument of perigee: | 55.2956° |
| revolutions per day: | 13.79047893 |
| mean anomaly at epoch: | 305.5351° |
| orbit number at epoch: | 6194 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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