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 40069U 14037A 24357.86928023 .00000348 00000-0 17900-3 0 9998
2 40069 98.4523 343.8424 0006015 159.2608 200.8815 14.21169307542428
Epoch (UTC): | 22 December 2024 20:51:45 |
Eccentricity: | 0.0006015 |
inclination: | 98.4523° |
perigee height: | 817 km |
apogee height: | 826 km |
right ascension of ascending node: | 343.8424° |
argument of perigee: | 159.2608° |
revolutions per day: | 14.21169307 |
mean anomaly at epoch: | 200.8815° |
orbit number at epoch: | 54242 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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