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 39769U 14029D 24358.19351895 .00012240 00000-0 12827-2 0 9994
2 39769 97.7173 66.9714 0002853 316.8245 43.2748 14.89700930572755
Epoch (UTC): | 23 December 2024 04:38:40 |
Eccentricity: | 0.0002853 |
inclination: | 97.7173° |
perigee height: | 597 km |
apogee height: | 601 km |
right ascension of ascending node: | 66.9714° |
argument of perigee: | 316.8245° |
revolutions per day: | 14.89700930 |
mean anomaly at epoch: | 43.2748° |
orbit number at epoch: | 57275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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