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 16012U 85079B 24282.73527717 .00001645 00000-0 56020-3 0 9998
2 16012 74.0567 275.6847 0015880 235.1654 124.8006 14.37221515 47258
Epoch (UTC): | 08 October 2024 17:38:47 |
Eccentricity: | 0.0015880 |
inclination: | 74.0567° |
perigee height: | 756 km |
apogee height: | 779 km |
right ascension of ascending node: | 275.6847° |
argument of perigee: | 235.1654° |
revolutions per day: | 14.37221515 |
mean anomaly at epoch: | 124.8006° |
orbit number at epoch: | 4725 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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