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 24262.81972514 .00000377 00000-0 19284-3 0 9991
2 40069 98.4449 252.9096 0007048 87.0158 273.1826 14.21062432528920
Epoch (UTC): | 18 September 2024 19:40:24 |
Eccentricity: | 0.0007048 |
inclination: | 98.4449° |
perigee height: | 816 km |
apogee height: | 827 km |
right ascension of ascending node: | 252.9096° |
argument of perigee: | 87.0158° |
revolutions per day: | 14.21062432 |
mean anomaly at epoch: | 273.1826° |
orbit number at epoch: | 52892 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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