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 43133U 18004Y 24082.99093794 .12081440 24922-5 34225-3 0 9996
2 43133 97.2664 174.2977 0012622 265.0607 94.9254 16.44332482345851
Epoch (UTC): | 22 March 2024 23:46:57 |
Eccentricity: | 0.0012622 |
inclination: | 97.2664° |
perigee height: | 146 km |
apogee height: | 162 km |
right ascension of ascending node: | 174.2977° |
argument of perigee: | 265.0607° |
revolutions per day: | 16.44332482 |
mean anomaly at epoch: | 94.9254° |
orbit number at epoch: | 34585 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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