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 00053U 60009E 22148.47791784 -.00000122 00000-0 -35707-3 0 9999
2 00053 47.2750 229.3483 0096910 19.1413 341.2980 12.17270501755055
Epoch (UTC): | 28 May 2022 11:28:12 |
Eccentricity: | 0.0096910 |
inclination: | 47.2750° |
perigee height: | 1527 km |
apogee height: | 1682 km |
right ascension of ascending node: | 229.3483° |
argument of perigee: | 19.1413° |
revolutions per day: | 12.17270501 |
mean anomaly at epoch: | 341.2980° |
orbit number at epoch: | 75505 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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