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 55690U 23025A 24358.17549674 .00015136 00000-0 63869-3 0 9993
2 55690 97.4043 71.1861 0003324 152.3084 207.8330 15.23375836101685
| Epoch (UTC): | 23 December 2024 04:12:42 |
| Eccentricity: | 0.0003324 |
| inclination: | 97.4043° |
| perigee height: | 493 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 71.1861° |
| argument of perigee: | 152.3084° |
| revolutions per day: | 15.23375836 |
| mean anomaly at epoch: | 207.8330° |
| orbit number at epoch: | 10168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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