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 40907U 15049J 22176.85577756 .00005661 00000-0 26686-3 0 9996
2 40907 97.4902 180.1879 0012264 333.4856 146.6087 15.19828421374247
Epoch (UTC): | 25 June 2022 20:32:19 |
Eccentricity: | 0.0012264 |
inclination: | 97.4902° |
perigee height: | 498 km |
apogee height: | 515 km |
right ascension of ascending node: | 180.1879° |
argument of perigee: | 333.4856° |
revolutions per day: | 15.19828421 |
mean anomaly at epoch: | 146.6087° |
orbit number at epoch: | 37424 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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