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 22180.85503925 .00001079 00000-0 13739-3 0 9993
2 39417 97.6368 151.7919 0057998 5.7182 354.4682 14.82382841464961
Epoch (UTC): | 29 June 2022 20:31:15 |
Eccentricity: | 0.0057998 |
inclination: | 97.6368° |
perigee height: | 581 km |
apogee height: | 662 km |
right ascension of ascending node: | 151.7919° |
argument of perigee: | 5.7182° |
revolutions per day: | 14.82382841 |
mean anomaly at epoch: | 354.4682° |
orbit number at epoch: | 46496 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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