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 40911U 15049N 23340.75626524 .00017788 00000-0 52089-3 0 9991
2 40911 97.4857 350.5615 0006747 265.2465 94.8008 15.35268218454773
Epoch (UTC): | 06 December 2023 18:09:01 |
Eccentricity: | 0.0006747 |
inclination: | 97.4857° |
perigee height: | 455 km |
apogee height: | 465 km |
right ascension of ascending node: | 350.5615° |
argument of perigee: | 265.2465° |
revolutions per day: | 15.35268218 |
mean anomaly at epoch: | 94.8008° |
orbit number at epoch: | 45477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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