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 43922U 19002A 24357.59271962 .00000468 00000-0 16006-3 0 9998
2 43922 86.3981 219.8922 0001999 83.6490 276.4934 14.34217790311365
| Epoch (UTC): | 22 December 2024 14:13:30 |
| Eccentricity: | 0.0001999 |
| inclination: | 86.3981° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 219.8922° |
| argument of perigee: | 83.6490° |
| revolutions per day: | 14.34217790 |
| mean anomaly at epoch: | 276.4934° |
| orbit number at epoch: | 31136 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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