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 23155.37682836 .00021867 00000-0 57837-3 0 9997
2 47311 60.6804 107.7631 0014200 169.7126 190.4262 15.38335735132313
Epoch (UTC): | 04 June 2023 09:02:37 |
Eccentricity: | 0.0014200 |
inclination: | 60.6804° |
perigee height: | 441 km |
apogee height: | 461 km |
right ascension of ascending node: | 107.7631° |
argument of perigee: | 169.7126° |
revolutions per day: | 15.38335735 |
mean anomaly at epoch: | 190.4262° |
orbit number at epoch: | 13231 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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