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 39132U 13015C 18116.14616344 .00000532 00000-0 47202-4 0 9993
2 39132 64.8800 3.4438 0027261 227.0302 292.7528 15.06964447275647
Epoch (UTC): | 26 April 2018 03:30:28 |
Eccentricity: | 0.0027261 |
inclination: | 64.8800° |
perigee height: | 526 km |
apogee height: | 564 km |
right ascension of ascending node: | 3.4438° |
argument of perigee: | 227.0302° |
revolutions per day: | 15.06964447 |
mean anomaly at epoch: | 292.7528° |
orbit number at epoch: | 27564 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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