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 40071U 14037C 23086.87956981 .00002968 00000-0 37500-3 0 9992
2 40071 98.3712 334.1746 0009089 121.0370 239.1740 14.82676737471326
Epoch (UTC): | 27 March 2023 21:06:34 |
Eccentricity: | 0.0009089 |
inclination: | 98.3712° |
perigee height: | 614 km |
apogee height: | 627 km |
right ascension of ascending node: | 334.1746° |
argument of perigee: | 121.0370° |
revolutions per day: | 14.82676737 |
mean anomaly at epoch: | 239.1740° |
orbit number at epoch: | 47132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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