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 23081.79268986 .00003154 00000-0 55803-3 0 9991
2 39430 97.7900 337.9491 0145198 246.4671 112.1199 14.61372418496928
Epoch (UTC): | 22 March 2023 19:01:28 |
Eccentricity: | 0.0145198 |
inclination: | 97.7900° |
perigee height: | 586 km |
apogee height: | 791 km |
right ascension of ascending node: | 337.9491° |
argument of perigee: | 246.4671° |
revolutions per day: | 14.61372418 |
mean anomaly at epoch: | 112.1199° |
orbit number at epoch: | 49692 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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