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 23087.90228491 .00007648 00000-0 98859-3 0 9990
2 40057 98.3736 277.3383 0010945 137.3189 222.8868 14.81181410471544
Epoch (UTC): | 28 March 2023 21:39:17 |
Eccentricity: | 0.0010945 |
inclination: | 98.3736° |
perigee height: | 618 km |
apogee height: | 633 km |
right ascension of ascending node: | 277.3383° |
argument of perigee: | 137.3189° |
revolutions per day: | 14.81181410 |
mean anomaly at epoch: | 222.8868° |
orbit number at epoch: | 47154 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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