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 18343.85746873 -.00000078 +00000-0 +00000-0 0 9999
2 26382 010.5678 035.8590 0006833 265.4113 082.4071 01.00103878067432
| Epoch (UTC): | 09 December 2018 20:34:45 |
| Eccentricity: | 0.0006833 |
| inclination: | 10.5678° |
| perigee height: | 35804 km |
| apogee height: | 35862 km |
| right ascension of ascending node: | 35.8590° |
| argument of perigee: | 265.4113° |
| revolutions per day: | 1.00103878 |
| mean anomaly at epoch: | 82.4071° |
| orbit number at epoch: | 6743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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