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 40100U 14043B 18136.88922947 0.00000000 00000-0 00000-0 0 08
2 40100 0.0980 93.8798 0001460 34.3784 325.6216 1.00000679 06
| Epoch (UTC): | 16 May 2018 21:20:29 |
| Eccentricity: | 0.0001460 |
| inclination: | 0.0980° |
| perigee height: | 35856 km |
| apogee height: | 35868 km |
| right ascension of ascending node: | 93.8798° |
| argument of perigee: | 34.3784° |
| revolutions per day: | 1.00000679 |
| mean anomaly at epoch: | 325.6216° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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