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 23091.17294578 .00003001 00000-0 53020-3 0 9990
2 39430 97.7879 346.7889 0145302 216.5805 142.5407 14.61437670498299
Epoch (UTC): | 01 April 2023 04:09:02 |
Eccentricity: | 0.0145302 |
inclination: | 97.7879° |
perigee height: | 586 km |
apogee height: | 791 km |
right ascension of ascending node: | 346.7889° |
argument of perigee: | 216.5805° |
revolutions per day: | 14.61437670 |
mean anomaly at epoch: | 142.5407° |
orbit number at epoch: | 49829 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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