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 40032U 14033Y 23148.08424262 .00002862 00000-0 28137-3 0 9998
2 40032 97.9663 88.3857 0010970 8.1594 351.9801 14.92917674485491
Epoch (UTC): | 28 May 2023 02:01:18 |
Eccentricity: | 0.0010970 |
inclination: | 97.9663° |
perigee height: | 581 km |
apogee height: | 596 km |
right ascension of ascending node: | 88.3857° |
argument of perigee: | 8.1594° |
revolutions per day: | 14.92917674 |
mean anomaly at epoch: | 351.9801° |
orbit number at epoch: | 48549 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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