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 61349U 24140VN 24357.47983194 .00007446 00000-0 13600-2 0 9993
2 61349 89.0799 335.9653 0146061 322.2881 36.8160 14.59119544 16098
| Epoch (UTC): | 22 December 2024 11:30:57 |
| Eccentricity: | 0.0146061 |
| inclination: | 89.0799° |
| perigee height: | 592 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 335.9653° |
| argument of perigee: | 322.2881° |
| revolutions per day: | 14.59119544 |
| mean anomaly at epoch: | 36.8160° |
| orbit number at epoch: | 1609 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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