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 23029.13747374 .00000005 00000-0 -29684-4 0 9992
2 44909 82.5190 80.3448 0218064 151.8407 209.4692 12.79717972144426
Epoch (UTC): | 29 January 2023 03:17:57 |
Eccentricity: | 0.0218064 |
inclination: | 82.5190° |
perigee height: | 1174 km |
apogee height: | 1511 km |
right ascension of ascending node: | 80.3448° |
argument of perigee: | 151.8407° |
revolutions per day: | 12.79717972 |
mean anomaly at epoch: | 209.4692° |
orbit number at epoch: | 14442 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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