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 22U 59009A 23085.18296932 .00007602 00000-0 53100-3 0 9992
2 22 50.2826 26.1079 0128679 171.4952 188.8220 14.99745198376828
| Epoch (UTC): | 26 March 2023 04:23:28 |
| Eccentricity: | 0.0128679 |
| inclination: | 50.2826° |
| perigee height: | 478 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 26.1079° |
| argument of perigee: | 171.4952° |
| revolutions per day: | 14.99745198 |
| mean anomaly at epoch: | 188.8220° |
| orbit number at epoch: | 37682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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