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 40931U 15052B 23155.26341798 .00001134 00000-0 67535-4 0 9995
2 40931 5.9985 178.7633 0012552 112.9184 247.2269 14.77226870415322
Epoch (UTC): | 04 June 2023 06:19:19 |
Eccentricity: | 0.0012552 |
inclination: | 5.9985° |
perigee height: | 629 km |
apogee height: | 647 km |
right ascension of ascending node: | 178.7633° |
argument of perigee: | 112.9184° |
revolutions per day: | 14.77226870 |
mean anomaly at epoch: | 247.2269° |
orbit number at epoch: | 41532 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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