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 22179.91003981 .00001211 00000-0 15334-3 0 9996
2 39417 97.6367 150.8895 0058096 8.7964 351.4253 14.82380719464822
Epoch (UTC): | 28 June 2022 21:50:27 |
Eccentricity: | 0.0058096 |
inclination: | 97.6367° |
perigee height: | 581 km |
apogee height: | 662 km |
right ascension of ascending node: | 150.8895° |
argument of perigee: | 8.7964° |
revolutions per day: | 14.82380719 |
mean anomaly at epoch: | 351.4253° |
orbit number at epoch: | 46482 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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