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 22175.86002390 .00001656 00000-0 20725-3 0 9992
2 39417 97.6364 147.0221 0058492 21.9610 338.4091 14.82368508464226
Epoch (UTC): | 24 June 2022 20:38:26 |
Eccentricity: | 0.0058492 |
inclination: | 97.6364° |
perigee height: | 581 km |
apogee height: | 663 km |
right ascension of ascending node: | 147.0221° |
argument of perigee: | 21.9610° |
revolutions per day: | 14.82368508 |
mean anomaly at epoch: | 338.4091° |
orbit number at epoch: | 46422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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