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 39440U 13066AA 23159.64696578 .00004082 00000-0 52779-3 0 9994
2 39440 97.7721 108.6778 0077007 55.8296 305.0186 14.79361205512894
Epoch (UTC): | 08 June 2023 15:31:37 |
Eccentricity: | 0.0077007 |
inclination: | 97.7721° |
perigee height: | 577 km |
apogee height: | 685 km |
right ascension of ascending node: | 108.6778° |
argument of perigee: | 55.8296° |
revolutions per day: | 14.79361205 |
mean anomaly at epoch: | 305.0186° |
orbit number at epoch: | 51289 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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