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 41744U 16052A 23076.80069444 .00000029 00000-0 00000+0 0 9997
2 41744 1.1479 93.5999 0004142 175.5803 11.1771 1.00327131 6831
Epoch (UTC): | 17 March 2023 19:13:00 |
Eccentricity: | 0.0004142 |
inclination: | 1.1479° |
perigee height: | 35753 km |
apogee height: | 35788 km |
right ascension of ascending node: | 93.5999° |
argument of perigee: | 175.5803° |
revolutions per day: | 1.00327131 |
mean anomaly at epoch: | 11.1771° |
orbit number at epoch: | 683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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