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 27386U 02009A 22186.96200731 .00000055 00000-0 31569-4 0 9992
2 27386 98.1838 167.2021 0001349 90.2142 332.9745 14.38136258 66195
| Epoch (UTC): | 05 July 2022 23:05:17 |
| Eccentricity: | 0.0001349 |
| inclination: | 98.1838° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 167.2021° |
| argument of perigee: | 90.2142° |
| revolutions per day: | 14.38136258 |
| mean anomaly at epoch: | 332.9745° |
| orbit number at epoch: | 6619 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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