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 14781U 84021B 23084.49059946 .00004047 00000-0 48535-3 0 9992
2 14781 97.6511 64.7179 0009833 112.5651 247.6606 14.84547809102723
Epoch (UTC): | 25 March 2023 11:46:27 |
Eccentricity: | 0.0009833 |
inclination: | 97.6511° |
perigee height: | 608 km |
apogee height: | 622 km |
right ascension of ascending node: | 64.7179° |
argument of perigee: | 112.5651° |
revolutions per day: | 14.84547809 |
mean anomaly at epoch: | 247.6606° |
orbit number at epoch: | 10272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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