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 39417U 13066B 22179.16753938 .00001298 00000-0 16397-3 0 9992
2 39417 97.6367 150.1805 0058171 11.2149 349.0346 14.82378780464713
Epoch (UTC): | 28 June 2022 04:01:15 |
Eccentricity: | 0.0058171 |
inclination: | 97.6367° |
perigee height: | 581 km |
apogee height: | 662 km |
right ascension of ascending node: | 150.1805° |
argument of perigee: | 11.2149° |
revolutions per day: | 14.82378780 |
mean anomaly at epoch: | 349.0346° |
orbit number at epoch: | 46471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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