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 24259.93215215 -.00000023 00000-0 54687-3 0 9996
2 23439 64.8137 257.0178 0147617 126.6093 234.8512 11.27578682223824
| Epoch (UTC): | 15 September 2024 22:22:17 |
| Eccentricity: | 0.0147617 |
| inclination: | 64.8137° |
| perigee height: | 1898 km |
| apogee height: | 2146 km |
| right ascension of ascending node: | 257.0178° |
| argument of perigee: | 126.6093° |
| revolutions per day: | 11.27578682 |
| mean anomaly at epoch: | 234.8512° |
| orbit number at epoch: | 22382 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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