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 40119U 14049B 24357.80466752 .00004005 00000-0 40947-3 0 9998
2 40119 97.8862 96.9539 0016252 102.2303 258.0736 14.91041626560663
Epoch (UTC): | 22 December 2024 19:18:43 |
Eccentricity: | 0.0016252 |
inclination: | 97.8862° |
perigee height: | 583 km |
apogee height: | 606 km |
right ascension of ascending node: | 96.9539° |
argument of perigee: | 102.2303° |
revolutions per day: | 14.91041626 |
mean anomaly at epoch: | 258.0736° |
orbit number at epoch: | 56066 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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