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 43937U 19003F 22179.54324317 .00007193 00000-0 24128-3 0 9999
2 43937 97.1290 212.4631 0022553 113.2170 247.1450 15.30930906191670
Epoch (UTC): | 28 June 2022 13:02:16 |
Eccentricity: | 0.0022553 |
inclination: | 97.1290° |
perigee height: | 457 km |
apogee height: | 488 km |
right ascension of ascending node: | 212.4631° |
argument of perigee: | 113.2170° |
revolutions per day: | 15.30930906 |
mean anomaly at epoch: | 247.1450° |
orbit number at epoch: | 19167 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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