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 40057U 14034E 22137.46215875 .00002352 00000-0 32567-3 0 9999
2 40057 98.3620 308.7826 0011755 71.8744 288.3769 14.78998203424891
Epoch (UTC): | 17 May 2022 11:05:30 |
Eccentricity: | 0.0011755 |
inclination: | 98.3620° |
perigee height: | 624 km |
apogee height: | 641 km |
right ascension of ascending node: | 308.7826° |
argument of perigee: | 71.8744° |
revolutions per day: | 14.78998203 |
mean anomaly at epoch: | 288.3769° |
orbit number at epoch: | 42489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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