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 40911U 15049N 23087.97119112 .00022424 00000-0 88293-3 0 9992
2 40911 97.4931 95.7758 0013505 81.7619 333.8237 15.25545569416127
Epoch (UTC): | 28 March 2023 23:18:30 |
Eccentricity: | 0.0013505 |
inclination: | 97.4931° |
perigee height: | 480 km |
apogee height: | 498 km |
right ascension of ascending node: | 95.7758° |
argument of perigee: | 81.7619° |
revolutions per day: | 15.25545569 |
mean anomaly at epoch: | 333.8237° |
orbit number at epoch: | 41612 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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