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 23081.38226005 .00248894 00000-0 94121-3 0 9990
2 40903 97.1269 148.4742 0006463 170.4364 318.4143 15.87051630422677
Epoch (UTC): | 22 March 2023 09:10:27 |
Eccentricity: | 0.0006463 |
inclination: | 97.1269° |
perigee height: | 306 km |
apogee height: | 315 km |
right ascension of ascending node: | 148.4742° |
argument of perigee: | 170.4364° |
revolutions per day: | 15.87051630 |
mean anomaly at epoch: | 318.4143° |
orbit number at epoch: | 42267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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