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 21019.55405014 .00000012 00000-0 17325-4 0 9999
2 27386 98.1418 21.2758 0001191 85.9515 23.0478 14.38009172989677
| Epoch (UTC): | 19 January 2021 13:17:49 |
| Eccentricity: | 0.0001191 |
| inclination: | 98.1418° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 21.2758° |
| argument of perigee: | 85.9515° |
| revolutions per day: | 14.38009172 |
| mean anomaly at epoch: | 23.0478° |
| orbit number at epoch: | 98967 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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