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 23088.82250544 .00007939 00000-0 78326-3 0 9998
2 40032 97.9609 28.4411 0010460 185.8513 174.2585 14.92225651476133
Epoch (UTC): | 29 March 2023 19:44:24 |
Eccentricity: | 0.0010460 |
inclination: | 97.9609° |
perigee height: | 584 km |
apogee height: | 598 km |
right ascension of ascending node: | 28.4411° |
argument of perigee: | 185.8513° |
revolutions per day: | 14.92225651 |
mean anomaly at epoch: | 174.2585° |
orbit number at epoch: | 47613 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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