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 26382U 00032A 19082.81368653 -.00000283 +00000-0 +00000-0 0 9990
2 26382 010.6797 035.0542 0006589 286.0719 083.2674 01.00079534068488
| Epoch (UTC): | 23 March 2019 19:31:42 |
| Eccentricity: | 0.0006589 |
| inclination: | 10.6797° |
| perigee height: | 35812 km |
| apogee height: | 35868 km |
| right ascension of ascending node: | 35.0542° |
| argument of perigee: | 286.0719° |
| revolutions per day: | 1.00079534 |
| mean anomaly at epoch: | 83.2674° |
| orbit number at epoch: | 6848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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