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 23158.52782817 .00000002 00000-0 -33191-4 0 9994
2 44909 82.5219 354.3659 0216888 209.3180 149.5609 12.79720910160926
Epoch (UTC): | 07 June 2023 12:40:04 |
Eccentricity: | 0.0216888 |
inclination: | 82.5219° |
perigee height: | 1175 km |
apogee height: | 1510 km |
right ascension of ascending node: | 354.3659° |
argument of perigee: | 209.3180° |
revolutions per day: | 12.79720910 |
mean anomaly at epoch: | 149.5609° |
orbit number at epoch: | 16092 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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