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 05435U 71071A 21023.60562790 -.00000052 00000-0 31563-4 0 9996
2 05435 50.1406 159.0335 0110279 203.6868 155.8960 14.55309193588638
Epoch (UTC): | 23 January 2021 14:32:06 |
Eccentricity: | 0.0110279 |
inclination: | 50.1406° |
perigee height: | 630 km |
apogee height: | 786 km |
right ascension of ascending node: | 159.0335° |
argument of perigee: | 203.6868° |
revolutions per day: | 14.55309193 |
mean anomaly at epoch: | 155.8960° |
orbit number at epoch: | 58863 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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