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 31949U 99025CNA 24354.72811684 .00000843 00000-0 41293-3 0 9993
2 31949 98.5184 348.9102 0127898 163.5610 196.9771 14.16099656904366
| Epoch (UTC): | 19 December 2024 17:28:29 |
| Eccentricity: | 0.0127898 |
| inclination: | 98.5184° |
| perigee height: | 746 km |
| apogee height: | 931 km |
| right ascension of ascending node: | 348.9102° |
| argument of perigee: | 163.5610° |
| revolutions per day: | 14.16099656 |
| mean anomaly at epoch: | 196.9771° |
| orbit number at epoch: | 90436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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