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 21020.03277021 .00000010 00000-0 16732-4 0 9998
2 27386 98.1418 21.7295 0001190 86.2149 339.5951 14.38009192989745
| Epoch (UTC): | 20 January 2021 00:47:11 |
| Eccentricity: | 0.0001190 |
| inclination: | 98.1418° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 21.7295° |
| argument of perigee: | 86.2149° |
| revolutions per day: | 14.38009192 |
| mean anomaly at epoch: | 339.5951° |
| orbit number at epoch: | 98974 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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