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 40906U 15049H 23160.09266260 .00012727 00000-0 49276-3 0 9991
2 40906 97.4936 167.2044 0011815 180.3961 179.7270 15.26252232427160
Epoch (UTC): | 09 June 2023 02:13:26 |
Eccentricity: | 0.0011815 |
inclination: | 97.4936° |
perigee height: | 479 km |
apogee height: | 495 km |
right ascension of ascending node: | 167.2044° |
argument of perigee: | 180.3961° |
revolutions per day: | 15.26252232 |
mean anomaly at epoch: | 179.7270° |
orbit number at epoch: | 42716 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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