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 23079.64299626 .00000019 00000-0 26554-4 0 9992
2 44909 82.5218 46.7711 0218222 34.2469 327.2486 12.79719249150835
Epoch (UTC): | 20 March 2023 15:25:54 |
Eccentricity: | 0.0218222 |
inclination: | 82.5218° |
perigee height: | 1174 km |
apogee height: | 1511 km |
right ascension of ascending node: | 46.7711° |
argument of perigee: | 34.2469° |
revolutions per day: | 12.79719249 |
mean anomaly at epoch: | 327.2486° |
orbit number at epoch: | 15083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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