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 20438U 90005C 18343.90289094 -.00000026 00000-0 75507-5 0 9999
2 20438 98.7867 300.0831 0010995 90.5709 334.4733 14.31025696507616
| Epoch (UTC): | 09 December 2018 21:40:09 |
| Eccentricity: | 0.0010995 |
| inclination: | 98.7867° |
| perigee height: | 780 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 300.0831° |
| argument of perigee: | 90.5709° |
| revolutions per day: | 14.31025696 |
| mean anomaly at epoch: | 334.4733° |
| orbit number at epoch: | 50761 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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