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 31739U 99025CEN 24358.00482244 .00000369 00000-0 18251-3 0 9992
2 31739 98.7985 50.8539 0128105 17.3769 343.1731 14.18952816908555
| Epoch (UTC): | 23 December 2024 00:06:56 |
| Eccentricity: | 0.0128105 |
| inclination: | 98.7985° |
| perigee height: | 736 km |
| apogee height: | 921 km |
| right ascension of ascending node: | 50.8539° |
| argument of perigee: | 17.3769° |
| revolutions per day: | 14.18952816 |
| mean anomaly at epoch: | 343.1731° |
| orbit number at epoch: | 90855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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