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 60235U 24128A 25188.94378471 .00001723 00000-0 15406-3 0 9992
2 60235 61.9953 346.6330 0059142 56.9956 303.6797 14.98852000 54367
Epoch (UTC): | 07 July 2025 22:39:02 |
Eccentricity: | 0.0059142 |
inclination: | 61.9953° |
perigee height: | 529 km |
apogee height: | 611 km |
right ascension of ascending node: | 346.6330° |
argument of perigee: | 56.9956° |
revolutions per day: | 14.98852000 |
mean anomaly at epoch: | 303.6797° |
orbit number at epoch: | 5436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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