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 11U 59001A 19201.20130200 .00000021 00000-0 -13105-6 0 9998
2 11 32.8659 226.4977 1467941 170.2624 192.9990 11.85613840577159
| Epoch (UTC): | 20 July 2019 04:49:52 |
| Eccentricity: | 0.1467941 |
| inclination: | 32.8659° |
| perigee height: | 553 km |
| apogee height: | 2938 km |
| right ascension of ascending node: | 226.4977° |
| argument of perigee: | 170.2624° |
| revolutions per day: | 11.85613840 |
| mean anomaly at epoch: | 192.9990° |
| orbit number at epoch: | 57715 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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