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 25567U 98072A 23088.86021116 .00000121 00000-0 11600-3 0 9992
2 25567 82.9472 233.5275 0026952 128.1970 341.1823 13.71916185216506
| Epoch (UTC): | 29 March 2023 20:38:42 |
| Eccentricity: | 0.0026952 |
| inclination: | 82.9472° |
| perigee height: | 973 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 233.5275° |
| argument of perigee: | 128.1970° |
| revolutions per day: | 13.71916185 |
| mean anomaly at epoch: | 341.1823° |
| orbit number at epoch: | 21650 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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