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 20401U 90001A 18173.46473050 -.00000092 +00000-0 +00000-0 0 9998
2 20401 013.3759 009.3904 0014329 254.1992 270.8158 00.98995640017899
| Epoch (UTC): | 22 June 2018 11:09:12 |
| Eccentricity: | 0.0014329 |
| inclination: | 13.3759° |
| perigee height: | 36087 km |
| apogee height: | 36209 km |
| right ascension of ascending node: | 9.3904° |
| argument of perigee: | 254.1992° |
| revolutions per day: | 0.98995640 |
| mean anomaly at epoch: | 270.8158° |
| orbit number at epoch: | 1789 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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