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 19922U 89028B 22225.21075830 .00000065 00000-0 50203-4 0 9994
2 19922 82.9581 109.8534 0036946 13.1413 347.0698 13.77257624676166
Epoch (UTC): | 13 August 2022 05:03:29 |
Eccentricity: | 0.0036946 |
inclination: | 82.9581° |
perigee height: | 946 km |
apogee height: | 1001 km |
right ascension of ascending node: | 109.8534° |
argument of perigee: | 13.1413° |
revolutions per day: | 13.77257624 |
mean anomaly at epoch: | 347.0698° |
orbit number at epoch: | 67616 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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