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 23080.13024203 .00015896 00000-0 65787-3 0 9991
2 40906 97.4969 87.1112 0014724 108.6622 316.6564 15.23930023414972
Epoch (UTC): | 21 March 2023 03:07:32 |
Eccentricity: | 0.0014724 |
inclination: | 97.4969° |
perigee height: | 484 km |
apogee height: | 504 km |
right ascension of ascending node: | 87.1112° |
argument of perigee: | 108.6622° |
revolutions per day: | 15.23930023 |
mean anomaly at epoch: | 316.6564° |
orbit number at epoch: | 41497 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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