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 40900U 15049B 22141.86769767 .00039445 00000-0 11715-2 0 9990
2 40900 97.4016 159.7258 0009937 38.1513 84.5667 15.34628380370532
Epoch (UTC): | 21 May 2022 20:49:29 |
Eccentricity: | 0.0009937 |
inclination: | 97.4016° |
perigee height: | 455 km |
apogee height: | 469 km |
right ascension of ascending node: | 159.7258° |
argument of perigee: | 38.1513° |
revolutions per day: | 15.34628380 |
mean anomaly at epoch: | 84.5667° |
orbit number at epoch: | 37053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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