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 00011U 59001A 23084.68737410 .00004683 00000-0 24748-2 0 9998
2 00011 32.8708 217.0357 1462447 202.8782 149.9579 11.86853816395068
Epoch (UTC): | 25 March 2023 16:29:49 |
Eccentricity: | 0.1462447 |
inclination: | 32.8708° |
perigee height: | 553 km |
apogee height: | 2927 km |
right ascension of ascending node: | 217.0357° |
argument of perigee: | 202.8782° |
revolutions per day: | 11.86853816 |
mean anomaly at epoch: | 149.9579° |
orbit number at epoch: | 39506 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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