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 22135.68705187 .00012088 00000-0 49447-3 0 9996
2 47311 60.6843 125.5444 0011661 295.6031 64.3852 15.24694627 73465
Epoch (UTC): | 15 May 2022 16:29:21 |
Eccentricity: | 0.0011661 |
inclination: | 60.6843° |
perigee height: | 483 km |
apogee height: | 500 km |
right ascension of ascending node: | 125.5444° |
argument of perigee: | 295.6031° |
revolutions per day: | 15.24694627 |
mean anomaly at epoch: | 64.3852° |
orbit number at epoch: | 7346 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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