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 24278U 96046B 24260.72847205 .00000079 00000-0 11896-3 0 9991
2 24278 98.5797 183.3798 0349294 311.2978 45.8570 13.53210397386810
| Epoch (UTC): | 16 September 2024 17:28:59 |
| Eccentricity: | 0.0349294 |
| inclination: | 98.5797° |
| perigee height: | 800 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 183.3798° |
| argument of perigee: | 311.2978° |
| revolutions per day: | 13.53210397 |
| mean anomaly at epoch: | 45.8570° |
| orbit number at epoch: | 38681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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