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 41918U 17003B 24258.81710352 .00001030 00000-0 36054-3 0 9997
2 41918 86.4030 356.0364 0001649 87.6544 272.4841 14.34219911401454
| Epoch (UTC): | 14 September 2024 19:36:37 |
| Eccentricity: | 0.0001649 |
| inclination: | 86.4030° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 356.0364° |
| argument of perigee: | 87.6544° |
| revolutions per day: | 14.34219911 |
| mean anomaly at epoch: | 272.4841° |
| orbit number at epoch: | 40145 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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