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 14032U 83037A 25198.48276003 .00142811 00000-0 56337-3 0 9990
2 14032 82.4912 12.3212 0003471 301.9688 58.1245 15.86433133311466
Epoch (UTC): | 17 July 2025 11:35:10 |
Eccentricity: | 0.0003471 |
inclination: | 82.4912° |
perigee height: | 310 km |
apogee height: | 314 km |
right ascension of ascending node: | 12.3212° |
argument of perigee: | 301.9688° |
revolutions per day: | 15.86433133 |
mean anomaly at epoch: | 58.1245° |
orbit number at epoch: | 31146 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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