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 40907U 15049J 23333.49541926 .00029499 00000-0 86260-3 0 9991
2 40907 97.4875 342.8717 0006986 297.7922 62.2612 15.35206687453780
Epoch (UTC): | 29 November 2023 11:53:24 |
Eccentricity: | 0.0006986 |
inclination: | 97.4875° |
perigee height: | 455 km |
apogee height: | 465 km |
right ascension of ascending node: | 342.8717° |
argument of perigee: | 297.7922° |
revolutions per day: | 15.35206687 |
mean anomaly at epoch: | 62.2612° |
orbit number at epoch: | 45378 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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