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 14096U 83051B 25198.47447393 .00000193 00000-0 35217-3 0 9997
2 14096 72.3008 350.3990 1093265 50.2424 318.9865 12.09943994860727
Epoch (UTC): | 17 July 2025 11:23:14 |
Eccentricity: | 0.1093265 |
inclination: | 72.3008° |
perigee height: | 760 km |
apogee height: | 2513 km |
right ascension of ascending node: | 350.3990° |
argument of perigee: | 50.2424° |
revolutions per day: | 12.09943994 |
mean anomaly at epoch: | 318.9865° |
orbit number at epoch: | 86072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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