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 39090U 13009E 23158.52426889 .00000326 00000-0 12796-3 0 9996
2 39090 98.3888 352.1511 0007790 297.4101 62.6292 14.35597648538333
Epoch (UTC): | 07 June 2023 12:34:56 |
Eccentricity: | 0.0007790 |
inclination: | 98.3888° |
perigee height: | 767 km |
apogee height: | 778 km |
right ascension of ascending node: | 352.1511° |
argument of perigee: | 297.4101° |
revolutions per day: | 14.35597648 |
mean anomaly at epoch: | 62.6292° |
orbit number at epoch: | 53833 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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