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 31702U 07027B 18111.85656999 0.00000000 00000-0 00000-0 0 01
2 31702 63.3626 43.1668 0319435 7.0752 352.9247 14.18624030 06
Epoch (UTC): | 21 April 2018 20:33:27 |
Eccentricity: | 0.0319435 |
inclination: | 63.3626° |
perigee height: | 600 km |
apogee height: | 1060 km |
right ascension of ascending node: | 43.1668° |
argument of perigee: | 7.0752° |
revolutions per day: | 14.18624030 |
mean anomaly at epoch: | 352.9247° |
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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