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 31755U 99025CFE 24358.22661059 .00002079 00000-0 10677-2 0 9990
2 31755 98.7633 353.8570 0190093 302.1158 116.9358 14.07540867912414
| Epoch (UTC): | 23 December 2024 05:26:19 |
| Eccentricity: | 0.0190093 |
| inclination: | 98.7633° |
| perigee height: | 730 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 353.8570° |
| argument of perigee: | 302.1158° |
| revolutions per day: | 14.07540867 |
| mean anomaly at epoch: | 116.9358° |
| orbit number at epoch: | 91241 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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