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 40908U 15049K 22137.53005742 .00003931 00000-0 20992-3 0 9992
2 40908 97.5156 138.4249 0016887 120.1066 338.9649 15.15587503367809
Epoch (UTC): | 17 May 2022 12:43:16 |
Eccentricity: | 0.0016887 |
inclination: | 97.5156° |
perigee height: | 507 km |
apogee height: | 531 km |
right ascension of ascending node: | 138.4249° |
argument of perigee: | 120.1066° |
revolutions per day: | 15.15587503 |
mean anomaly at epoch: | 338.9649° |
orbit number at epoch: | 36780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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