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 55909U 23035B 23339.57571557 .00002501 00000-0 23980-3 0 9996
2 55909 44.0026 4.8733 0008622 15.5403 344.5716 14.95633539 39401
| Epoch (UTC): | 05 December 2023 13:49:01 |
| Eccentricity: | 0.0008622 |
| inclination: | 44.0026° |
| perigee height: | 574 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 4.8733° |
| argument of perigee: | 15.5403° |
| revolutions per day: | 14.95633539 |
| mean anomaly at epoch: | 344.5716° |
| orbit number at epoch: | 3940 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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