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 22184.93712647 .00000045 00000-0 28394-4 0 9992
2 27386 98.1838 165.2721 0001342 90.1618 295.7301 14.38135869 65831
| Epoch (UTC): | 03 July 2022 22:29:27 |
| Eccentricity: | 0.0001342 |
| inclination: | 98.1838° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 165.2721° |
| argument of perigee: | 90.1618° |
| revolutions per day: | 14.38135869 |
| mean anomaly at epoch: | 295.7301° |
| orbit number at epoch: | 6583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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