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 54307U 22151BA 23333.55473527 .00017551 00000-0 49699-2 0 9990
2 54307 98.6100 343.4028 0115178 257.7426 101.0846 14.41747195 54366
Epoch (UTC): | 29 November 2023 13:18:49 |
Eccentricity: | 0.0115178 |
inclination: | 98.6100° |
perigee height: | 670 km |
apogee height: | 835 km |
right ascension of ascending node: | 343.4028° |
argument of perigee: | 257.7426° |
revolutions per day: | 14.41747195 |
mean anomaly at epoch: | 101.0846° |
orbit number at epoch: | 5436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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