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 25193.47209155 .00000197 00000-0 77214-4 0 9999
2 23561 98.4826 262.7650 0007687 135.0986 235.9933 14.39548017584681
| Epoch (UTC): | 12 July 2025 11:19:48 |
| Eccentricity: | 0.0007687 |
| inclination: | 98.4826° |
| perigee height: | 754 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 262.7650° |
| argument of perigee: | 135.0986° |
| revolutions per day: | 14.39548017 |
| mean anomaly at epoch: | 235.9933° |
| orbit number at epoch: | 58468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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