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 18262.89824281 .00000025 00000-0 00000+0 0 9994
2 20401 13.3794 8.6022 0015999 252.7099 106.6995 0.98996198100883
| Epoch (UTC): | 19 September 2018 21:33:28 |
| Eccentricity: | 0.0015999 |
| inclination: | 13.3794° |
| perigee height: | 36079 km |
| apogee height: | 36215 km |
| right ascension of ascending node: | 8.6022° |
| argument of perigee: | 252.7099° |
| revolutions per day: | 0.98996198 |
| mean anomaly at epoch: | 106.6995° |
| orbit number at epoch: | 10088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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