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 26483U 00051A 18113.85317130 .00000056 00000-0 00000+0 0 9991
2 26483 64.8623 99.9893 0148715 258.1319 347.9218 1.64981857 68711
Epoch (UTC): | 23 April 2018 20:28:34 |
Eccentricity: | 0.0148715 |
inclination: | 64.8623° |
perigee height: | 23425 km |
apogee height: | 24325 km |
right ascension of ascending node: | 99.9893° |
argument of perigee: | 258.1319° |
revolutions per day: | 1.64981857 |
mean anomaly at epoch: | 347.9218° |
orbit number at epoch: | 6871 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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