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 45589C 20025BL 21020.01060447 .00006398 00000-0 43800-3 0 206
2 45589 52.9956 212.3791 0002376 89.7633 31.9356 15.05590336 13
Epoch (UTC): | 20 January 2021 00:15:16 |
Eccentricity: | 0.0002376 |
inclination: | 52.9956° |
perigee height: | 548 km |
apogee height: | 551 km |
right ascension of ascending node: | 212.3791° |
argument of perigee: | 89.7633° |
revolutions per day: | 15.05590336 |
mean anomaly at epoch: | 31.9356° |
orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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