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 40186U 11077K 24282.45882660 -.00000100 00000-0 00000-0 0 9994
2 40186 25.7551 243.1790 7301428 348.0496 21.1967 1.88721094 87473
Epoch (UTC): | 08 October 2024 11:00:42 |
Eccentricity: | 0.7301428 |
inclination: | 25.7551° |
perigee height: | 1086 km |
apogee height: | 41477 km |
right ascension of ascending node: | 243.1790° |
argument of perigee: | 348.0496° |
revolutions per day: | 1.88721094 |
mean anomaly at epoch: | 21.1967° |
orbit number at epoch: | 8747 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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