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 25189.34036156 .00002990 00000-0 10287-3 0 9994
2 53807 53.2298 202.3975 0006626 185.9340 174.1586 15.33348379157362
| Epoch (UTC): | 08 July 2025 08:10:07 |
| Eccentricity: | 0.0006626 |
| inclination: | 53.2298° |
| perigee height: | 461 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 202.3975° |
| argument of perigee: | 185.9340° |
| revolutions per day: | 15.33348379 |
| mean anomaly at epoch: | 174.1586° |
| orbit number at epoch: | 15736 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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