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 24277.18328239 .00000818 00000-0 39587-3 0 9994
2 40069 98.4464 266.6465 0006744 52.2039 307.9748 14.21077147530968
Epoch (UTC): | 03 October 2024 04:23:55 |
Eccentricity: | 0.0006744 |
inclination: | 98.4464° |
perigee height: | 817 km |
apogee height: | 826 km |
right ascension of ascending node: | 266.6465° |
argument of perigee: | 52.2039° |
revolutions per day: | 14.21077147 |
mean anomaly at epoch: | 307.9748° |
orbit number at epoch: | 53096 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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