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 20775U 90078B 25312.83801693 .00021464 00000-0 66244-3 0 9998
2 20775 82.9069 359.6035 0381932 59.2909 304.5351 14.84095353791345
| Epoch (UTC): | 08 November 2025 20:06:44 |
| Eccentricity: | 0.0381932 |
| inclination: | 82.9069° |
| perigee height: | 349 km |
| apogee height: | 883 km |
| right ascension of ascending node: | 359.6035° |
| argument of perigee: | 59.2909° |
| revolutions per day: | 14.84095353 |
| mean anomaly at epoch: | 304.5351° |
| orbit number at epoch: | 79134 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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