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 23088.68477911 .00006981 00000-0 33363-3 0 9999
2 53807 53.1990 76.7814 0012867 160.6349 199.5139 15.20054093 30355
| Epoch (UTC): | 29 March 2023 16:26:04 |
| Eccentricity: | 0.0012867 |
| inclination: | 53.1990° |
| perigee height: | 497 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 76.7814° |
| argument of perigee: | 160.6349° |
| revolutions per day: | 15.20054093 |
| mean anomaly at epoch: | 199.5139° |
| orbit number at epoch: | 3035 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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