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 55057U 23001BA 23335.70612732 .00020675 00000-0 89765-3 0 9990
2 55057 97.4575 33.9815 0012202 143.2773 216.9301 15.22278830 50537
| Epoch (UTC): | 01 December 2023 16:56:49 |
| Eccentricity: | 0.0012202 |
| inclination: | 97.4575° |
| perigee height: | 490 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 33.9815° |
| argument of perigee: | 143.2773° |
| revolutions per day: | 15.22278830 |
| mean anomaly at epoch: | 216.9301° |
| orbit number at epoch: | 5053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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