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 22175.53979167 .00000019 00000-0 37136-4 0 9999
2 44909 82.5211 225.5678 0216348 303.3503 54.7053 12.79713566116417
Epoch (UTC): | 24 June 2022 12:57:18 |
Eccentricity: | 0.0216348 |
inclination: | 82.5211° |
perigee height: | 1175 km |
apogee height: | 1509 km |
right ascension of ascending node: | 225.5678° |
argument of perigee: | 303.3503° |
revolutions per day: | 12.79713566 |
mean anomaly at epoch: | 54.7053° |
orbit number at epoch: | 11641 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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