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 46U 60007B 24255.48960395 .00005740 00000-0 11143-2 0 9993
2 46 66.6902 180.6676 0194481 55.2830 306.6426 14.52518076363418
| Epoch (UTC): | 11 September 2024 11:45:01 |
| Eccentricity: | 0.0194481 |
| inclination: | 66.6902° |
| perigee height: | 579 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 180.6676° |
| argument of perigee: | 55.2830° |
| revolutions per day: | 14.52518076 |
| mean anomaly at epoch: | 306.6426° |
| orbit number at epoch: | 36341 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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