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 25159U 98007C 24280.14800110 .00006370 00000-0 23304-2 0 9997
2 25159 107.9677 337.2416 0042921 327.4344 32.4149 14.33299196387910
| Epoch (UTC): | 06 October 2024 03:33:07 |
| Eccentricity: | 0.0042921 |
| inclination: | 107.9677° |
| perigee height: | 750 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 337.2416° |
| argument of perigee: | 327.4344° |
| revolutions per day: | 14.33299196 |
| mean anomaly at epoch: | 32.4149° |
| orbit number at epoch: | 38791 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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