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 23153.75181771 .00001452 00000-0 18607-3 0 9995
2 40071 98.3623 44.1217 0006750 272.4494 87.5945 14.82944290481143
Epoch (UTC): | 02 June 2023 18:02:37 |
Eccentricity: | 0.0006750 |
inclination: | 98.3623° |
perigee height: | 615 km |
apogee height: | 625 km |
right ascension of ascending node: | 44.1217° |
argument of perigee: | 272.4494° |
revolutions per day: | 14.82944290 |
mean anomaly at epoch: | 87.5945° |
orbit number at epoch: | 48114 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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