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 50U 60009B 19051.80850454 -.00000057 +00000-0 +26161-3 0 9992
2 50 047.2299 179.2324 0113294 327.1616 032.2170 12.20106739611299
Epoch (UTC): | 20 February 2019 19:24:14 |
Eccentricity: | 0.0113294 |
inclination: | 47.2299° |
perigee height: | 1502 km |
apogee height: | 1682 km |
right ascension of ascending node: | 179.2324° |
argument of perigee: | 327.1616° |
revolutions per day: | 12.20106739 |
mean anomaly at epoch: | 32.2170° |
orbit number at epoch: | 61129 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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