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 23405U 94077B 24255.56095802 .00000557 00000-0 31001-3 0 9999
2 23405 70.9829 57.1282 0004748 271.2684 88.7895 14.15424693539505
Epoch (UTC): | 11 September 2024 13:27:46 |
Eccentricity: | 0.0004748 |
inclination: | 70.9829° |
perigee height: | 837 km |
apogee height: | 844 km |
right ascension of ascending node: | 57.1282° |
argument of perigee: | 271.2684° |
revolutions per day: | 14.15424693 |
mean anomaly at epoch: | 88.7895° |
orbit number at epoch: | 53950 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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