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 51659U 22013D 23155.59077011 .00006641 00000-0 30021-3 0 9996
2 51659 97.5600 169.5452 0031780 124.8985 235.5244 15.20821039 72121
Epoch (UTC): | 04 June 2023 14:10:42 |
Eccentricity: | 0.0031780 |
inclination: | 97.5600° |
perigee height: | 481 km |
apogee height: | 525 km |
right ascension of ascending node: | 169.5452° |
argument of perigee: | 124.8985° |
revolutions per day: | 15.20821039 |
mean anomaly at epoch: | 235.5244° |
orbit number at epoch: | 7212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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