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 25194.06577556 .00128271 00000-0 53539-3 0 9992
2 14032 82.4895 17.1726 0002856 323.5501 36.5574 15.85294269310760
Epoch (UTC): | 13 July 2025 01:34:43 |
Eccentricity: | 0.0002856 |
inclination: | 82.4895° |
perigee height: | 313 km |
apogee height: | 317 km |
right ascension of ascending node: | 17.1726° |
argument of perigee: | 323.5501° |
revolutions per day: | 15.85294269 |
mean anomaly at epoch: | 36.5574° |
orbit number at epoch: | 31076 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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