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 41557U 16033B 23294.57261523 .13570584 25586-5 20126-3 0 9994
2 41557 97.3596 50.5245 0012741 279.5777 80.4087 16.47966609413529
| Epoch (UTC): | 21 October 2023 13:44:33 |
| Eccentricity: | 0.0012741 |
| inclination: | 97.3596° |
| perigee height: | 136 km |
| apogee height: | 153 km |
| right ascension of ascending node: | 50.5245° |
| argument of perigee: | 279.5777° |
| revolutions per day: | 16.47966609 |
| mean anomaly at epoch: | 80.4087° |
| orbit number at epoch: | 41352 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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