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 35517U 86019VQ 24353.21288800 .00000861 00000-0 65209-3 0 9991
2 35517 98.8133 164.8954 0381703 271.7937 83.9540 13.67047979 69535
| Epoch (UTC): | 18 December 2024 05:06:33 |
| Eccentricity: | 0.0381703 |
| inclination: | 98.8133° |
| perigee height: | 728 km |
| apogee height: | 1292 km |
| right ascension of ascending node: | 164.8954° |
| argument of perigee: | 271.7937° |
| revolutions per day: | 13.67047979 |
| mean anomaly at epoch: | 83.9540° |
| orbit number at epoch: | 6953 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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