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 41619U 16040W 23083.35671806 .00276388 00000-0 52434-2 0 9998
2 41619 97.1719 132.9745 0007557 177.9241 182.2042 15.47258862363709
Epoch (UTC): | 24 March 2023 08:33:40 |
Eccentricity: | 0.0007557 |
inclination: | 97.1719° |
perigee height: | 419 km |
apogee height: | 430 km |
right ascension of ascending node: | 132.9745° |
argument of perigee: | 177.9241° |
revolutions per day: | 15.47258862 |
mean anomaly at epoch: | 182.2042° |
orbit number at epoch: | 36370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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