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 04589U 70086B 24276.87375373 .00002153 00000-0 65376-3 0 9992
2 04589 74.0593 67.6918 0020917 328.4064 31.5835 14.42647972830753
| Epoch (UTC): | 02 October 2024 20:58:12 |
| Eccentricity: | 0.0020917 |
| inclination: | 74.0593° |
| perigee height: | 735 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 67.6918° |
| argument of perigee: | 328.4064° |
| revolutions per day: | 14.42647972 |
| mean anomaly at epoch: | 31.5835° |
| orbit number at epoch: | 83075 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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