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 28414U 04035B 21019.14150226 .00000416 00000-0 43990-4 0 9995
2 28414 97.7499 42.1719 0005145 336.0557 24.0431 14.94304315891145
Epoch (UTC): | 19 January 2021 03:23:45 |
Eccentricity: | 0.0005145 |
inclination: | 97.7499° |
perigee height: | 581 km |
apogee height: | 588 km |
right ascension of ascending node: | 42.1719° |
argument of perigee: | 336.0557° |
revolutions per day: | 14.94304315 |
mean anomaly at epoch: | 24.0431° |
orbit number at epoch: | 89114 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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