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 26064U 00004D 18168.83256916 -.00000020 00000-0 13373-4 0 9990
2 26064 100.1948 240.4653 0037883 13.8542 346.3669 14.36157589963586
| Epoch (UTC): | 17 June 2018 19:58:53 |
| Eccentricity: | 0.0037883 |
| inclination: | 100.1948° |
| perigee height: | 744 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 240.4653° |
| argument of perigee: | 13.8542° |
| revolutions per day: | 14.36157589 |
| mean anomaly at epoch: | 346.3669° |
| orbit number at epoch: | 96358 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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