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 22U 59009A 19016.18813609 -.00000031 00000-0 21383-4 0 9996
2 22 50.2846 13.0500 0140338 79.1742 282.4964 14.94735659147795
| Epoch (UTC): | 16 January 2019 04:30:54 |
| Eccentricity: | 0.0140338 |
| inclination: | 50.2846° |
| perigee height: | 485 km |
| apogee height: | 681 km |
| right ascension of ascending node: | 13.0500° |
| argument of perigee: | 79.1742° |
| revolutions per day: | 14.94735659 |
| mean anomaly at epoch: | 282.4964° |
| orbit number at epoch: | 14779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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