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 22135.91007039 .00006370 00000-0 30529-3 0 9994
2 40911 97.4908 140.1575 0015157 107.6647 316.7317 15.19167759367912
Epoch (UTC): | 15 May 2022 21:50:30 |
Eccentricity: | 0.0015157 |
inclination: | 97.4908° |
perigee height: | 498 km |
apogee height: | 519 km |
right ascension of ascending node: | 140.1575° |
argument of perigee: | 107.6647° |
revolutions per day: | 15.19167759 |
mean anomaly at epoch: | 316.7317° |
orbit number at epoch: | 36791 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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