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 40479U 95015BX 24358.00805158 .00002494 00000-0 11766-2 0 9995
2 40479 98.7858 10.1846 0003746 142.5071 217.6368 14.20728975508541
| Epoch (UTC): | 23 December 2024 00:11:35 |
| Eccentricity: | 0.0003746 |
| inclination: | 98.7858° |
| perigee height: | 820 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 10.1846° |
| argument of perigee: | 142.5071° |
| revolutions per day: | 14.20728975 |
| mean anomaly at epoch: | 217.6368° |
| orbit number at epoch: | 50854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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