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 19080.24357887 -.00000153 00000-0 00000+0 0 9998
2 20401 13.3754 7.0642 0015309 273.5876 274.4756 0.98996765102688
| Epoch (UTC): | 21 March 2019 05:50:45 |
| Eccentricity: | 0.0015309 |
| inclination: | 13.3754° |
| perigee height: | 36082 km |
| apogee height: | 36212 km |
| right ascension of ascending node: | 7.0642° |
| argument of perigee: | 273.5876° |
| revolutions per day: | 0.98996765 |
| mean anomaly at epoch: | 274.4756° |
| orbit number at epoch: | 10268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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