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 23092.15814687 .00006686 00000-0 86427-3 0 9990
2 40057 98.3732 281.7830 0011096 125.4045 234.8201 14.81233622472170
Epoch (UTC): | 02 April 2023 03:47:43 |
Eccentricity: | 0.0011096 |
inclination: | 98.3732° |
perigee height: | 617 km |
apogee height: | 633 km |
right ascension of ascending node: | 281.7830° |
argument of perigee: | 125.4045° |
revolutions per day: | 14.81233622 |
mean anomaly at epoch: | 234.8201° |
orbit number at epoch: | 47217 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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