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 42729U 98067MJ 19037.76010169 .18316134 12568-4 56330-3 0 9997
2 42729 51.6029 213.2858 0007111 290.6627 69.5057 16.44582755 97544
Epoch (UTC): | 06 February 2019 18:14:32 |
Eccentricity: | 0.0007111 |
inclination: | 51.6029° |
perigee height: | 149 km |
apogee height: | 158 km |
right ascension of ascending node: | 213.2858° |
argument of perigee: | 290.6627° |
revolutions per day: | 16.44582755 |
mean anomaly at epoch: | 69.5057° |
orbit number at epoch: | 9754 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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