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 39417U 13066B 23078.86069268 .00004632 00000-0 54613-3 0 9992
2 39417 97.6752 43.7613 0054365 219.7426 139.9801 14.84159302503949
Epoch (UTC): | 19 March 2023 20:39:23 |
Eccentricity: | 0.0054365 |
inclination: | 97.6752° |
perigee height: | 578 km |
apogee height: | 654 km |
right ascension of ascending node: | 43.7613° |
argument of perigee: | 219.7426° |
revolutions per day: | 14.84159302 |
mean anomaly at epoch: | 139.9801° |
orbit number at epoch: | 50394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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