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 44909U 19096E 23078.86119212 .00000019 00000-0 29896-4 0 9999
2 44909 82.5216 47.2905 0218244 36.0676 325.4926 12.79719217150731
Epoch (UTC): | 19 March 2023 20:40:06 |
Eccentricity: | 0.0218244 |
inclination: | 82.5216° |
perigee height: | 1174 km |
apogee height: | 1511 km |
right ascension of ascending node: | 47.2905° |
argument of perigee: | 36.0676° |
revolutions per day: | 12.79719217 |
mean anomaly at epoch: | 325.4926° |
orbit number at epoch: | 15073 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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