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 40900U 15049B 23081.37474519 .01017267 47227-3 26996-2 0 9999
2 40900 97.3555 110.6951 0003755 192.1242 294.3286 15.94712583417622
Epoch (UTC): | 22 March 2023 08:59:37 |
Eccentricity: | 0.0003755 |
inclination: | 97.3555° |
perigee height: | 286 km |
apogee height: | 291 km |
right ascension of ascending node: | 110.6951° |
argument of perigee: | 192.1242° |
revolutions per day: | 15.94712583 |
mean anomaly at epoch: | 294.3286° |
orbit number at epoch: | 41762 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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