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 9904U 77024B 21061.50225534 .00000071 00000-0 34107-4 0 9995
2 9904 81.2589 261.1579 0054981 113.2453 247.4518 14.06900974253230
Epoch (UTC): | 02 March 2021 12:03:14 |
Eccentricity: | 0.0054981 |
inclination: | 81.2589° |
perigee height: | 830 km |
apogee height: | 910 km |
right ascension of ascending node: | 261.1579° |
argument of perigee: | 113.2453° |
revolutions per day: | 14.06900974 |
mean anomaly at epoch: | 247.4518° |
orbit number at epoch: | 25323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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