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 21020.52833916 .00000015 00000-0 18460-4 0 9998
2 27386 98.1418 22.1992 0001194 86.4300 23.3639 14.38009263989817
| Epoch (UTC): | 20 January 2021 12:40:48 |
| Eccentricity: | 0.0001194 |
| inclination: | 98.1418° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 22.1992° |
| argument of perigee: | 86.4300° |
| revolutions per day: | 14.38009263 |
| mean anomaly at epoch: | 23.3639° |
| orbit number at epoch: | 98981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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