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 23090.38322942 .00384213 58721-4 11215-2 0 9992
2 40903 97.1224 157.9125 0005488 165.9393 322.8242 15.92790838424100
Epoch (UTC): | 31 March 2023 09:11:51 |
Eccentricity: | 0.0005488 |
inclination: | 97.1224° |
perigee height: | 291 km |
apogee height: | 298 km |
right ascension of ascending node: | 157.9125° |
argument of perigee: | 165.9393° |
revolutions per day: | 15.92790838 |
mean anomaly at epoch: | 322.8242° |
orbit number at epoch: | 42410 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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