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 10777U 78034B 24357.53595376 .00000043 00000-0 27029-4 0 9999
2 10777 82.9426 348.3848 0027434 68.7571 80.5635 13.77652319348317
| Epoch (UTC): | 22 December 2024 12:51:46 |
| Eccentricity: | 0.0027434 |
| inclination: | 82.9426° |
| perigee height: | 952 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 348.3848° |
| argument of perigee: | 68.7571° |
| revolutions per day: | 13.77652319 |
| mean anomaly at epoch: | 80.5635° |
| orbit number at epoch: | 34831 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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