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 35703U 93036APY 23328.67678134 .00006791 00000-0 96452-3 0 9991
2 35703 74.0493 82.5930 0090813 351.1696 8.7873 14.74282976555183
| Epoch (UTC): | 24 November 2023 16:14:33 |
| Eccentricity: | 0.0090813 |
| inclination: | 74.0493° |
| perigee height: | 583 km |
| apogee height: | 711 km |
| right ascension of ascending node: | 82.5930° |
| argument of perigee: | 351.1696° |
| revolutions per day: | 14.74282976 |
| mean anomaly at epoch: | 8.7873° |
| orbit number at epoch: | 55518 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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