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 25131.83482576 .00005572 00000-0 48700-3 0 9996
2 39417 97.7790 89.0110 0045545 145.6869 214.7309 14.96375189620610
Epoch (UTC): | 11 May 2025 20:02:08 |
Eccentricity: | 0.0045545 |
inclination: | 97.7790° |
perigee height: | 546 km |
apogee height: | 610 km |
right ascension of ascending node: | 89.0110° |
argument of perigee: | 145.6869° |
revolutions per day: | 14.96375189 |
mean anomaly at epoch: | 214.7309° |
orbit number at epoch: | 62061 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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