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 40012U 14033C 24340.39602733 .00008518 00000-0 10354-2 0 9991
2 40012 97.7189 136.3605 0051022 105.5522 255.1332 14.82786928563183
Epoch (UTC): | 05 December 2024 09:30:16 |
Eccentricity: | 0.0051022 |
inclination: | 97.7189° |
perigee height: | 585 km |
apogee height: | 656 km |
right ascension of ascending node: | 136.3605° |
argument of perigee: | 105.5522° |
revolutions per day: | 14.82786928 |
mean anomaly at epoch: | 255.1332° |
orbit number at epoch: | 56318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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