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 14064U 83044A 25139.84790514 .00009589 00000-0 39018-3 0 9997
2 14064 64.9929 259.3645 0067446 319.0807 40.5271 15.22918414156991
Epoch (UTC): | 19 May 2025 20:20:59 |
Eccentricity: | 0.0067446 |
inclination: | 64.9929° |
perigee height: | 450 km |
apogee height: | 543 km |
right ascension of ascending node: | 259.3645° |
argument of perigee: | 319.0807° |
revolutions per day: | 15.22918414 |
mean anomaly at epoch: | 40.5271° |
orbit number at epoch: | 15699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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