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 40906U 15049H 23088.00173951 .00019170 00000-0 78541-3 0 9991
2 40906 97.4972 94.9837 0014620 85.4900 300.6108 15.24230693416170
Epoch (UTC): | 29 March 2023 00:02:30 |
Eccentricity: | 0.0014620 |
inclination: | 97.4972° |
perigee height: | 483 km |
apogee height: | 503 km |
right ascension of ascending node: | 94.9837° |
argument of perigee: | 85.4900° |
revolutions per day: | 15.24230693 |
mean anomaly at epoch: | 300.6108° |
orbit number at epoch: | 41617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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