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 42761U 17034D 23033.56308867 .00007054 00000-0 38813-3 0 9991
2 42761 43.0157 141.0710 0012011 307.9749 170.4970 15.14461555311213
Epoch (UTC): | 02 February 2023 13:30:50 |
Eccentricity: | 0.0012011 |
inclination: | 43.0157° |
perigee height: | 514 km |
apogee height: | 531 km |
right ascension of ascending node: | 141.0710° |
argument of perigee: | 307.9749° |
revolutions per day: | 15.14461555 |
mean anomaly at epoch: | 170.4970° |
orbit number at epoch: | 31121 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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