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 19109.06027927 .00000008 00000-0 16240-4 0 9995
2 27386 98.1545 133.1709 0001414 90.6150 326.5193 14.37946218897485
| Epoch (UTC): | 19 April 2019 01:26:48 |
| Eccentricity: | 0.0001414 |
| inclination: | 98.1545° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 133.1709° |
| argument of perigee: | 90.6150° |
| revolutions per day: | 14.37946218 |
| mean anomaly at epoch: | 326.5193° |
| orbit number at epoch: | 89748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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