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 14059U 83042B 24282.38999133 .00000875 00000-0 83803-3 0 9994
2 14059 82.9706 239.4995 0041733 327.5410 32.3182 13.78991963 83437
| Epoch (UTC): | 08 October 2024 09:21:35 |
| Eccentricity: | 0.0041733 |
| inclination: | 82.9706° |
| perigee height: | 937 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 239.4995° |
| argument of perigee: | 327.5410° |
| revolutions per day: | 13.78991963 |
| mean anomaly at epoch: | 32.3182° |
| orbit number at epoch: | 8343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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