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 19046.72584062 .00000011 00000-0 17244-4 0 9995
2 27386 98.1611 73.9678 0001168 95.9623 28.6896 14.37941368888520
| Epoch (UTC): | 15 February 2019 17:25:12 |
| Eccentricity: | 0.0001168 |
| inclination: | 98.1611° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 73.9678° |
| argument of perigee: | 95.9623° |
| revolutions per day: | 14.37941368 |
| mean anomaly at epoch: | 28.6896° |
| orbit number at epoch: | 88852 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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