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 35869U 09049E 18116.03815080 .00000002 00000-0 19644-4 0 9995
2 35869 98.4022 127.6634 0003711 324.1709 35.9221 14.22390476446649
| Epoch (UTC): | 26 April 2018 00:54:56 |
| Eccentricity: | 0.0003711 |
| inclination: | 98.4022° |
| perigee height: | 814 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 127.6634° |
| argument of perigee: | 324.1709° |
| revolutions per day: | 14.22390476 |
| mean anomaly at epoch: | 35.9221° |
| orbit number at epoch: | 44664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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