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 04157U 69082Z 23333.38222516 .00011908 00000-0 15400-2 0 9996
2 04157 70.0179 318.8630 0031113 42.8085 317.5480 14.80721925855182
| Epoch (UTC): | 29 November 2023 09:10:24 |
| Eccentricity: | 0.0031113 |
| inclination: | 70.0179° |
| perigee height: | 605 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 318.8630° |
| argument of perigee: | 42.8085° |
| revolutions per day: | 14.80721925 |
| mean anomaly at epoch: | 317.5480° |
| orbit number at epoch: | 85518 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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