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 23705U 95058B 24281.83245092 .00000229 00000-0 14149-3 0 9999
2 23705 71.0226 187.4052 0013153 199.5838 160.4781 14.15384009494874
| Epoch (UTC): | 07 October 2024 19:58:43 |
| Eccentricity: | 0.0013153 |
| inclination: | 71.0226° |
| perigee height: | 831 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 187.4052° |
| argument of perigee: | 199.5838° |
| revolutions per day: | 14.15384009 |
| mean anomaly at epoch: | 160.4781° |
| orbit number at epoch: | 49487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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