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 28480U 04046B 21065.84033005 .00000054 00000-0 35350-4 0 9992
2 28480 98.0570 86.0899 0142200 167.4250 5.5081 14.25743430847806
Epoch (UTC): | 06 March 2021 20:10:04 |
Eccentricity: | 0.0142200 |
inclination: | 98.0570° |
perigee height: | 704 km |
apogee height: | 908 km |
right ascension of ascending node: | 86.0899° |
argument of perigee: | 167.4250° |
revolutions per day: | 14.25743430 |
mean anomaly at epoch: | 5.5081° |
orbit number at epoch: | 84780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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