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 41558U 16033C 22268.57117756 .00013659 00000-0 35762-3 0 9995
2 41558 97.4119 12.8627 0009928 14.0260 114.7696 15.38784013353031
| Epoch (UTC): | 25 September 2022 13:42:29 |
| Eccentricity: | 0.0009928 |
| inclination: | 97.4119° |
| perigee height: | 443 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 12.8627° |
| argument of perigee: | 14.0260° |
| revolutions per day: | 15.38784013 |
| mean anomaly at epoch: | 114.7696° |
| orbit number at epoch: | 35303 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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