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 14059U 83042B 24282.17231855 .00000901 00000-0 86284-3 0 9997
2 14059 82.9706 239.6613 0041756 328.1347 31.7286 13.78991791 83669
Epoch (UTC): | 08 October 2024 04:08:08 |
Eccentricity: | 0.0041756 |
inclination: | 82.9706° |
perigee height: | 937 km |
apogee height: | 998 km |
right ascension of ascending node: | 239.6613° |
argument of perigee: | 328.1347° |
revolutions per day: | 13.78991791 |
mean anomaly at epoch: | 31.7286° |
orbit number at epoch: | 8366 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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