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 22175.81330123 .00024734 00000-0 69904-3 0 9991
2 40900 97.4000 193.8291 0006937 251.9757 195.0721 15.36310482375743
Epoch (UTC): | 24 June 2022 19:31:09 |
Eccentricity: | 0.0006937 |
inclination: | 97.4000° |
perigee height: | 452 km |
apogee height: | 462 km |
right ascension of ascending node: | 193.8291° |
argument of perigee: | 251.9757° |
revolutions per day: | 15.36310482 |
mean anomaly at epoch: | 195.0721° |
orbit number at epoch: | 37574 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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