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 23344.75708287 .00000030 00000-0 68969-4 0 9996
2 44909 82.5221 230.6107 0218110 133.9459 227.9869 12.79724341184741
Epoch (UTC): | 10 December 2023 18:10:11 |
Eccentricity: | 0.0218110 |
inclination: | 82.5221° |
perigee height: | 1174 km |
apogee height: | 1511 km |
right ascension of ascending node: | 230.6107° |
argument of perigee: | 133.9459° |
revolutions per day: | 12.79724341 |
mean anomaly at epoch: | 227.9869° |
orbit number at epoch: | 18474 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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