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 115U 60002D 25137.99591702 .00004644 00000-0 43902-3 0 9994
2 115 48.1625 240.2340 0028523 280.6466 79.1239 14.94926952480107
Epoch (UTC): | 17 May 2025 23:54:07 |
Eccentricity: | 0.0028523 |
inclination: | 48.1625° |
perigee height: | 563 km |
apogee height: | 602 km |
right ascension of ascending node: | 240.2340° |
argument of perigee: | 280.6466° |
revolutions per day: | 14.94926952 |
mean anomaly at epoch: | 79.1239° |
orbit number at epoch: | 48010 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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