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 47311U 21002C 22176.79326343 .00005874 00000-0 24053-3 0 9997
2 47311 60.6858 330.8494 0017695 342.8294 17.2193 15.25419557 79735
Epoch (UTC): | 25 June 2022 19:02:17 |
Eccentricity: | 0.0017695 |
inclination: | 60.6858° |
perigee height: | 477 km |
apogee height: | 501 km |
right ascension of ascending node: | 330.8494° |
argument of perigee: | 342.8294° |
revolutions per day: | 15.25419557 |
mean anomaly at epoch: | 17.2193° |
orbit number at epoch: | 7973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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