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 23155.89655207 .00010829 00000-0 42113-3 0 9990
2 40906 97.4928 162.9958 0011288 195.0514 165.0390 15.26154235426522
Epoch (UTC): | 04 June 2023 21:31:02 |
Eccentricity: | 0.0011288 |
inclination: | 97.4928° |
perigee height: | 479 km |
apogee height: | 495 km |
right ascension of ascending node: | 162.9958° |
argument of perigee: | 195.0514° |
revolutions per day: | 15.26154235 |
mean anomaly at epoch: | 165.0390° |
orbit number at epoch: | 42652 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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