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 43941U 19004A 24287.18329085 0.00027500 00000-0 39497-3 0 06
2 43941 73.5650 56.1233 0019687 225.2161 134.7838 15.55739962 05
Epoch (UTC): | 13 October 2024 04:23:56 |
Eccentricity: | 0.0019687 |
inclination: | 73.5650° |
perigee height: | 386 km |
apogee height: | 413 km |
right ascension of ascending node: | 56.1233° |
argument of perigee: | 225.2161° |
revolutions per day: | 15.55739962 |
mean anomaly at epoch: | 134.7838° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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