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 39430U 13066Q 22175.71835090 .00001690 00000-0 30809-3 0 9994
2 39430 97.8095 82.5020 0150085 22.5380 338.2325 14.60209619457353
Epoch (UTC): | 24 June 2022 17:14:25 |
Eccentricity: | 0.0150085 |
inclination: | 97.8095° |
perigee height: | 586 km |
apogee height: | 798 km |
right ascension of ascending node: | 82.5020° |
argument of perigee: | 22.5380° |
revolutions per day: | 14.60209619 |
mean anomaly at epoch: | 338.2325° |
orbit number at epoch: | 45735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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