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 11086U 78100C 22223.49083615 -.00000013 00000-0 -27316-3 0 9997
2 11086 82.5489 119.5032 0011314 259.0802 218.9054 11.96735696912757
| Epoch (UTC): | 11 August 2022 11:46:48 |
| Eccentricity: | 0.0011314 |
| inclination: | 82.5489° |
| perigee height: | 1686 km |
| apogee height: | 1704 km |
| right ascension of ascending node: | 119.5032° |
| argument of perigee: | 259.0802° |
| revolutions per day: | 11.96735696 |
| mean anomaly at epoch: | 218.9054° |
| orbit number at epoch: | 91275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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