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 40071U 14037C 23090.86123818 .00002594 00000-0 32858-3 0 9997
2 40071 98.3703 338.3413 0009316 110.1638 250.0573 14.82696015471914
Epoch (UTC): | 31 March 2023 20:40:10 |
Eccentricity: | 0.0009316 |
inclination: | 98.3703° |
perigee height: | 614 km |
apogee height: | 627 km |
right ascension of ascending node: | 338.3413° |
argument of perigee: | 110.1638° |
revolutions per day: | 14.82696015 |
mean anomaly at epoch: | 250.0573° |
orbit number at epoch: | 47191 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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