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 53807U 22111AL 25119.18838405 .00007727 00000-0 25449-3 0 9995
2 53807 53.2313 169.0693 0007553 350.6947 9.3914 15.32449796146603
| Epoch (UTC): | 29 April 2025 04:31:16 |
| Eccentricity: | 0.0007553 |
| inclination: | 53.2313° |
| perigee height: | 463 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 169.0693° |
| argument of perigee: | 350.6947° |
| revolutions per day: | 15.32449796 |
| mean anomaly at epoch: | 9.3914° |
| orbit number at epoch: | 14660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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