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 23439U 94085A 25166.82966631 -.00000061 00000-0 -52374-3 0 9991
2 23439 64.8127 175.6992 0145606 73.1211 288.5621 11.27581441254598
Epoch (UTC): | 15 June 2025 19:54:43 |
Eccentricity: | 0.0145606 |
inclination: | 64.8127° |
perigee height: | 1900 km |
apogee height: | 2144 km |
right ascension of ascending node: | 175.6992° |
argument of perigee: | 73.1211° |
revolutions per day: | 11.27581441 |
mean anomaly at epoch: | 288.5621° |
orbit number at epoch: | 25459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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