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 14372U 83099A 18109.33547397 .00000580 00000-0 26823-4 0 9994
2 14372 82.5176 40.9486 0017036 100.2447 21.1027 15.17940535884232
Epoch (UTC): | 19 April 2018 08:03:04 |
Eccentricity: | 0.0017036 |
inclination: | 82.5176° |
perigee height: | 500 km |
apogee height: | 524 km |
right ascension of ascending node: | 40.9486° |
argument of perigee: | 100.2447° |
revolutions per day: | 15.17940535 |
mean anomaly at epoch: | 21.1027° |
orbit number at epoch: | 88423 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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