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 23334.11520857 .00000263 00000-0 14094-3 0 9990
2 40069 98.4284 332.4256 0005067 210.3519 149.7366 14.20849543487218
Epoch (UTC): | 30 November 2023 02:45:54 |
Eccentricity: | 0.0005067 |
inclination: | 98.4284° |
perigee height: | 819 km |
apogee height: | 826 km |
right ascension of ascending node: | 332.4256° |
argument of perigee: | 210.3519° |
revolutions per day: | 14.20849543 |
mean anomaly at epoch: | 149.7366° |
orbit number at epoch: | 48721 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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