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 is defined by the following mean orbital elements,
1 20775U 26162.49537720 +.00000000 +00000-0 +54013-3 0 00004
2 20775 82.9014 166.7865 0352191 57.6230 305.8559 14.92097617 01
| Epoch (UTC): | 11 June 2026 11:53:20 |
| Eccentricity: | 0.0352191 |
| inclination: | 82.9014° |
| perigee height: | 346 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 166.7865° |
| argument of perigee: | 57.6230° |
| revolutions per day: | 14.92097617 |
| mean anomaly at epoch: | 305.8559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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