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 23439U 94085A 24357.66804219 -.00000037 00000-0 14416-3 0 9994
2 23439 64.8170 98.9635 0146061 107.4924 254.2021 11.27580325234845
| Epoch (UTC): | 22 December 2024 16:01:58 |
| Eccentricity: | 0.0146061 |
| inclination: | 64.8170° |
| perigee height: | 1899 km |
| apogee height: | 2145 km |
| right ascension of ascending node: | 98.9635° |
| argument of perigee: | 107.4924° |
| revolutions per day: | 11.27580325 |
| mean anomaly at epoch: | 254.2021° |
| orbit number at epoch: | 23484 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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