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 24262.86508790 .00129247 00000-0 12006-2 0 9994
2 40907 97.4626 286.5512 0001083 287.5913 72.5229 15.67020312499277
Epoch (UTC): | 18 September 2024 20:45:43 |
Eccentricity: | 0.0001083 |
inclination: | 97.4626° |
perigee height: | 367 km |
apogee height: | 368 km |
right ascension of ascending node: | 286.5512° |
argument of perigee: | 287.5913° |
revolutions per day: | 15.67020312 |
mean anomaly at epoch: | 72.5229° |
orbit number at epoch: | 49927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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