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 14679U 84010A 18116.72866185 .00000036 00000-0 21862-4 0 9992
2 14679 82.9608 193.5246 0041835 358.0869 112.6194 13.75088151686476
Epoch (UTC): | 26 April 2018 17:29:16 |
Eccentricity: | 0.0041835 |
inclination: | 82.9608° |
perigee height: | 950 km |
apogee height: | 1012 km |
right ascension of ascending node: | 193.5246° |
argument of perigee: | 358.0869° |
revolutions per day: | 13.75088151 |
mean anomaly at epoch: | 112.6194° |
orbit number at epoch: | 68647 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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