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 13719U 82116B 18116.21691302 .00000010 00000-0 -17344-5 0 9996
2 13719 81.2566 53.7137 0071494 178.9171 289.4282 14.14621698824625
Epoch (UTC): | 26 April 2018 05:12:21 |
Eccentricity: | 0.0071494 |
inclination: | 81.2566° |
perigee height: | 792 km |
apogee height: | 895 km |
right ascension of ascending node: | 53.7137° |
argument of perigee: | 178.9171° |
revolutions per day: | 14.14621698 |
mean anomaly at epoch: | 289.4282° |
orbit number at epoch: | 82462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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