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 39429U 13066P 25082.91887487 .00010112 00000-0 14162-2 0 9993
2 39429 97.7238 320.2893 0122145 41.8616 319.1854 14.72638692604653
Epoch (UTC): | 23 March 2025 22:03:10 |
Eccentricity: | 0.0122145 |
inclination: | 97.7238° |
perigee height: | 567 km |
apogee height: | 738 km |
right ascension of ascending node: | 320.2893° |
argument of perigee: | 41.8616° |
revolutions per day: | 14.72638692 |
mean anomaly at epoch: | 319.1854° |
orbit number at epoch: | 60465 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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