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 26094U 00004M 18175.26742573 .00000033 00000-0 27835-4 0 9998
2 26094 100.1903 296.0353 0033633 220.7873 139.0792 14.42435288964621
| Epoch (UTC): | 24 June 2018 06:25:05 |
| Eccentricity: | 0.0033633 |
| inclination: | 100.1903° |
| perigee height: | 726 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 296.0353° |
| argument of perigee: | 220.7873° |
| revolutions per day: | 14.42435288 |
| mean anomaly at epoch: | 139.0792° |
| orbit number at epoch: | 96462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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