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 41604U 16040F 23028.68319785 .00006719 00000-0 25843-3 0 9996
2 41604 97.1837 69.5226 0012552 60.7036 299.5456 15.26638454366794
| Epoch (UTC): | 28 January 2023 16:23:48 |
| Eccentricity: | 0.0012552 |
| inclination: | 97.1837° |
| perigee height: | 477 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 69.5226° |
| argument of perigee: | 60.7036° |
| revolutions per day: | 15.26638454 |
| mean anomaly at epoch: | 299.5456° |
| orbit number at epoch: | 36679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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