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 39430U 13066Q 23086.99637388 .00003988 00000-0 70252-3 0 9994
2 39430 97.7893 342.8531 0145001 229.9907 128.8504 14.61416456497689
Epoch (UTC): | 27 March 2023 23:54:46 |
Eccentricity: | 0.0145001 |
inclination: | 97.7893° |
perigee height: | 586 km |
apogee height: | 791 km |
right ascension of ascending node: | 342.8531° |
argument of perigee: | 229.9907° |
revolutions per day: | 14.61416456 |
mean anomaly at epoch: | 128.8504° |
orbit number at epoch: | 49768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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