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 21103.22350500 0.00001400 00000-0 52205-4 0 00
2 32750 98.2082 303.6579 0000221 109.8326 290.2684 15.27459184 02
Epoch (UTC): | 13 April 2021 05:21:50 |
Eccentricity: | 0.0000221 |
inclination: | 98.2082° |
perigee height: | 483 km |
apogee height: | 483 km |
right ascension of ascending node: | 303.6579° |
argument of perigee: | 109.8326° |
revolutions per day: | 15.27459184 |
mean anomaly at epoch: | 290.2684° |
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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