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 24279.70439693 .00013860 00000-0 17333-2 0 9990
2 40012 97.7157 77.8151 0050424 304.9228 54.7253 14.81504955554199
Epoch (UTC): | 05 October 2024 16:54:19 |
Eccentricity: | 0.0050424 |
inclination: | 97.7157° |
perigee height: | 589 km |
apogee height: | 660 km |
right ascension of ascending node: | 77.8151° |
argument of perigee: | 304.9228° |
revolutions per day: | 14.81504955 |
mean anomaly at epoch: | 54.7253° |
orbit number at epoch: | 55419 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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