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 05435U 71071A 23338.07359446 .00001806 00000-0 41007-3 0 9990
2 05435 50.1393 220.5553 0107293 37.4252 323.4088 14.56998428740798
| Epoch (UTC): | 04 December 2023 01:45:58 |
| Eccentricity: | 0.0107293 |
| inclination: | 50.1393° |
| perigee height: | 627 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 220.5553° |
| argument of perigee: | 37.4252° |
| revolutions per day: | 14.56998428 |
| mean anomaly at epoch: | 323.4088° |
| orbit number at epoch: | 74079 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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