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 19348.79847300 .00000009 00000-0 16288-4 0 9998
2 27386 98.1409 0.5820 0001329 89.7776 82.9956 14.37965836931939
| Epoch (UTC): | 14 December 2019 19:09:48 |
| Eccentricity: | 0.0001329 |
| inclination: | 98.1409° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 0.5820° |
| argument of perigee: | 89.7776° |
| revolutions per day: | 14.37965836 |
| mean anomaly at epoch: | 82.9956° |
| orbit number at epoch: | 93193 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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