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 4394U 70037B 24299.51796145 .99999999 -14140-5 66514-3 0 9994
2 4394 81.1936 58.2036 0012784 306.3071 180.0358 16.57086830977389
Epoch (UTC): | 25 October 2024 12:25:51 |
Eccentricity: | 0.0012784 |
inclination: | 81.1936° |
perigee height: | 112 km |
apogee height: | 129 km |
right ascension of ascending node: | 58.2036° |
argument of perigee: | 306.3071° |
revolutions per day: | 16.57086830 |
mean anomaly at epoch: | 180.0358° |
orbit number at epoch: | 97738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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