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 35869U 09049E 17290.47474921 .00000011 00000-0 23395-4 0 9998
2 35869 98.4101 305.9103 0005332 136.8838 223.2759 14.22377344419558
| Epoch (UTC): | 17 October 2017 11:23:38 |
| Eccentricity: | 0.0005332 |
| inclination: | 98.4101° |
| perigee height: | 813 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 305.9103° |
| argument of perigee: | 136.8838° |
| revolutions per day: | 14.22377344 |
| mean anomaly at epoch: | 223.2759° |
| orbit number at epoch: | 41955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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