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 37755U 11037A 22142.35827133 -.00000822 00000-0 00000-0 0 9995
2 37755 33.0094 308.3089 9085840 353.9599 359.1906 0.10655101 4350
Epoch (UTC): | 22 May 2022 08:35:54 |
Eccentricity: | 0.9085840 |
inclination: | 33.0094° |
perigee height: | 10803 km |
apogee height: | 352326 km |
right ascension of ascending node: | 308.3089° |
argument of perigee: | 353.9599° |
revolutions per day: | 0.10655101 |
mean anomaly at epoch: | 359.1906° |
orbit number at epoch: | 435 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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