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 19340.14451758 .00000019 00000-0 19617-4 0 9997
2 27386 98.1417 352.3811 0001334 91.3799 308.7607 14.37964961930698
| Epoch (UTC): | 06 December 2019 03:28:06 |
| Eccentricity: | 0.0001334 |
| inclination: | 98.1417° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 352.3811° |
| argument of perigee: | 91.3799° |
| revolutions per day: | 14.37964961 |
| mean anomaly at epoch: | 308.7607° |
| orbit number at epoch: | 93069 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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