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 41634U 16043A 22144.80087007 .00001349 00000-0 15685-3 0 9990
2 41634 75.0034 191.7435 0006988 27.7807 332.3745 14.86148612320149
Epoch (UTC): | 24 May 2022 19:13:15 |
Eccentricity: | 0.0006988 |
inclination: | 75.0034° |
perigee height: | 605 km |
apogee height: | 615 km |
right ascension of ascending node: | 191.7435° |
argument of perigee: | 27.7807° |
revolutions per day: | 14.86148612 |
mean anomaly at epoch: | 332.3745° |
orbit number at epoch: | 32014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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