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 22279.78440493 .00019019 00000-0 64644-3 0 9995
2 43133 97.3590 353.0804 0007160 337.2586 22.8337 15.30482999263310
| Epoch (UTC): | 06 October 2022 18:49:32 |
| Eccentricity: | 0.0007160 |
| inclination: | 97.3590° |
| perigee height: | 469 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 353.0804° |
| argument of perigee: | 337.2586° |
| revolutions per day: | 15.30482999 |
| mean anomaly at epoch: | 22.8337° |
| orbit number at epoch: | 26331 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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