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 23339.20610067 .00000014 00000-0 56546-5 0 9999
2 44909 82.5225 234.2975 0217935 146.8811 214.6156 12.79724262184033
Epoch (UTC): | 05 December 2023 04:56:47 |
Eccentricity: | 0.0217935 |
inclination: | 82.5225° |
perigee height: | 1174 km |
apogee height: | 1511 km |
right ascension of ascending node: | 234.2975° |
argument of perigee: | 146.8811° |
revolutions per day: | 12.79724262 |
mean anomaly at epoch: | 214.6156° |
orbit number at epoch: | 18403 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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