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 33498U 09002G 21015.93741130 .00000210 00000-0 35685-4 0 9999
2 33498 98.2350 252.5245 0011997 113.4798 246.7674 14.79260963644918
Epoch (UTC): | 15 January 2021 22:29:52 |
Eccentricity: | 0.0011997 |
inclination: | 98.2350° |
perigee height: | 623 km |
apogee height: | 640 km |
right ascension of ascending node: | 252.5245° |
argument of perigee: | 113.4798° |
revolutions per day: | 14.79260963 |
mean anomaly at epoch: | 246.7674° |
orbit number at epoch: | 64491 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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