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 37855U 11061F 22176.31038572 .00006547 00000-0 28897-3 0 9993
2 37855 101.7096 299.5423 0152681 38.8620 322.3456 15.12533149582428
Epoch (UTC): | 25 June 2022 07:26:57 |
Eccentricity: | 0.0152681 |
inclination: | 101.7096° |
perigee height: | 423 km |
apogee height: | 634 km |
right ascension of ascending node: | 299.5423° |
argument of perigee: | 38.8620° |
revolutions per day: | 15.12533149 |
mean anomaly at epoch: | 322.3456° |
orbit number at epoch: | 58242 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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