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 24255.32809268 .00009291 00000-0 94720-3 0 9997
2 115 48.1641 14.0127 0031796 249.1552 110.5958 14.90789688442944
Epoch (UTC): | 11 September 2024 07:52:27 |
Eccentricity: | 0.0031796 |
inclination: | 48.1641° |
perigee height: | 573 km |
apogee height: | 617 km |
right ascension of ascending node: | 14.0127° |
argument of perigee: | 249.1552° |
revolutions per day: | 14.90789688 |
mean anomaly at epoch: | 110.5958° |
orbit number at epoch: | 44294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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