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 10565U 77121G 24357.84899534 .00000448 00000-0 61775-3 0 9991
2 10565 65.8295 291.5447 0110080 142.2069 252.3454 13.65636950335246
| Epoch (UTC): | 22 December 2024 20:22:33 |
| Eccentricity: | 0.0110080 |
| inclination: | 65.8295° |
| perigee height: | 934 km |
| apogee height: | 1096 km |
| right ascension of ascending node: | 291.5447° |
| argument of perigee: | 142.2069° |
| revolutions per day: | 13.65636950 |
| mean anomaly at epoch: | 252.3454° |
| orbit number at epoch: | 33524 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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