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 24277.84745920 -.00000046 00000-0 -98740-4 0 9992
2 23439 64.8154 228.0431 0147254 123.1156 238.3999 11.27578842225842
| Epoch (UTC): | 03 October 2024 20:20:20 |
| Eccentricity: | 0.0147254 |
| inclination: | 64.8154° |
| perigee height: | 1898 km |
| apogee height: | 2146 km |
| right ascension of ascending node: | 228.0431° |
| argument of perigee: | 123.1156° |
| revolutions per day: | 11.27578842 |
| mean anomaly at epoch: | 238.3999° |
| orbit number at epoch: | 22584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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