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 37658U 78026JV 24357.49673904 .00000894 00000-0 64246-3 0 9991
2 37658 99.2420 244.7268 0067146 96.8837 28.5114 13.98563406 96983
| Epoch (UTC): | 22 December 2024 11:55:18 |
| Eccentricity: | 0.0067146 |
| inclination: | 99.2420° |
| perigee height: | 850 km |
| apogee height: | 947 km |
| right ascension of ascending node: | 244.7268° |
| argument of perigee: | 96.8837° |
| revolutions per day: | 13.98563406 |
| mean anomaly at epoch: | 28.5114° |
| orbit number at epoch: | 9698 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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