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 23343.19342800 .00000016 00000-0 12142-4 0 9994
2 44909 82.5222 231.6493 0218077 137.5752 224.2441 12.79724313184542
Epoch (UTC): | 09 December 2023 04:38:32 |
Eccentricity: | 0.0218077 |
inclination: | 82.5222° |
perigee height: | 1174 km |
apogee height: | 1511 km |
right ascension of ascending node: | 231.6493° |
argument of perigee: | 137.5752° |
revolutions per day: | 12.79724313 |
mean anomaly at epoch: | 224.2441° |
orbit number at epoch: | 18454 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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