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 40903U 15049E 23090.63936537 .00389031 60356-4 11238-2 0 9996
2 40903 97.1227 158.1825 0005412 165.5826 350.9657 15.92991487424146
Epoch (UTC): | 31 March 2023 15:20:41 |
Eccentricity: | 0.0005412 |
inclination: | 97.1227° |
perigee height: | 290 km |
apogee height: | 297 km |
right ascension of ascending node: | 158.1825° |
argument of perigee: | 165.5826° |
revolutions per day: | 15.92991487 |
mean anomaly at epoch: | 350.9657° |
orbit number at epoch: | 42414 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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