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 18199.50758637 -.00000273 +00000-0 +00000-0 0 9998
2 26382 010.4062 036.9949 0005254 260.8884 277.2604 01.00070935065990
| Epoch (UTC): | 18 July 2018 12:10:55 |
| Eccentricity: | 0.0005254 |
| inclination: | 10.4062° |
| perigee height: | 35820 km |
| apogee height: | 35865 km |
| right ascension of ascending node: | 36.9949° |
| argument of perigee: | 260.8884° |
| revolutions per day: | 1.00070935 |
| mean anomaly at epoch: | 277.2604° |
| orbit number at epoch: | 6599 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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