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 22141.76573791 .00000033 00000-0 84099-4 0 9996
2 44909 82.5224 248.0013 0217609 22.4220 338.6216 12.79713293112092
Epoch (UTC): | 21 May 2022 18:22:39 |
Eccentricity: | 0.0217609 |
inclination: | 82.5224° |
perigee height: | 1174 km |
apogee height: | 1510 km |
right ascension of ascending node: | 248.0013° |
argument of perigee: | 22.4220° |
revolutions per day: | 12.79713293 |
mean anomaly at epoch: | 338.6216° |
orbit number at epoch: | 11209 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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