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 23271.42282522 .00006177 00000-0 28102-3 0 9999
2 53807 53.2125 320.6314 0012448 18.2490 341.8952 15.21973111 58168
| Epoch (UTC): | 28 September 2023 10:08:52 |
| Eccentricity: | 0.0012448 |
| inclination: | 53.2125° |
| perigee height: | 491 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 320.6314° |
| argument of perigee: | 18.2490° |
| revolutions per day: | 15.21973111 |
| mean anomaly at epoch: | 341.8952° |
| orbit number at epoch: | 5816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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