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 32750U 08014A 21058.73787586 0.00001500 00000-0 55436-4 0 03
2 32750 98.2082 254.6981 0003103 70.0819 289.9180 15.27749295 03
Epoch (UTC): | 27 February 2021 17:42:32 |
Eccentricity: | 0.0003103 |
inclination: | 98.2082° |
perigee height: | 480 km |
apogee height: | 484 km |
right ascension of ascending node: | 254.6981° |
argument of perigee: | 70.0819° |
revolutions per day: | 15.27749295 |
mean anomaly at epoch: | 289.9180° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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