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 33499U 09002H 22137.19387477 .00001095 00000-0 16684-3 0 9993
2 33499 98.2221 18.7155 0010259 59.5355 300.6866 14.75962749716063
Epoch (UTC): | 17 May 2022 04:39:10 |
Eccentricity: | 0.0010259 |
inclination: | 98.2221° |
perigee height: | 635 km |
apogee height: | 649 km |
right ascension of ascending node: | 18.7155° |
argument of perigee: | 59.5355° |
revolutions per day: | 14.75962749 |
mean anomaly at epoch: | 300.6866° |
orbit number at epoch: | 71606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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