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 39765U 14028E 18140.41812354 +.00000023 +00000-0 +34903-4 0 9995
2 39765 082.4399 084.0154 0230919 086.7705 275.9794 12.83341910186994
| Epoch (UTC): | 20 May 2018 10:02:05 |
| Eccentricity: | 0.0230919 |
| inclination: | 82.4399° |
| perigee height: | 1150 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 84.0154° |
| argument of perigee: | 86.7705° |
| revolutions per day: | 12.83341910 |
| mean anomaly at epoch: | 275.9794° |
| orbit number at epoch: | 18699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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