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 23561U 95021B 25194.44506821 .00000205 00000-0 79573-4 0 9997
2 23561 98.4826 263.7281 0007726 132.6265 237.8820 14.39548554584827
| Epoch (UTC): | 13 July 2025 10:40:53 |
| Eccentricity: | 0.0007726 |
| inclination: | 98.4826° |
| perigee height: | 754 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 263.7281° |
| argument of perigee: | 132.6265° |
| revolutions per day: | 14.39548554 |
| mean anomaly at epoch: | 237.8820° |
| orbit number at epoch: | 58482 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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