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 00877U 64053B 21063.84109551 -.00000085 00000-0 81024-5 0 9999
2 00877 65.0769 288.0223 0081810 292.3283 66.9159 14.59420158999494
Epoch (UTC): | 04 March 2021 20:11:10 |
Eccentricity: | 0.0081810 |
inclination: | 65.0769° |
perigee height: | 637 km |
apogee height: | 753 km |
right ascension of ascending node: | 288.0223° |
argument of perigee: | 292.3283° |
revolutions per day: | 14.59420158 |
mean anomaly at epoch: | 66.9159° |
orbit number at epoch: | 99949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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