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 42983U 98067NF 18115.48167737 .00003544 00000-0 57089-4 0 9994
2 42983 51.6393 280.0704 0004193 7.9134 352.1923 15.55897493 28019
Epoch (UTC): | 25 April 2018 11:33:36 |
Eccentricity: | 0.0004193 |
inclination: | 51.6393° |
perigee height: | 397 km |
apogee height: | 402 km |
right ascension of ascending node: | 280.0704° |
argument of perigee: | 7.9134° |
revolutions per day: | 15.55897493 |
mean anomaly at epoch: | 352.1923° |
orbit number at epoch: | 2801 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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