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 10674U 78018A 23331.44867927 -.00000012 00000-0 60263-4 0 9996
2 10674 69.3626 331.9845 0161548 37.1568 113.9854 13.43655308245336
| Epoch (UTC): | 27 November 2023 10:46:05 |
| Eccentricity: | 0.0161548 |
| inclination: | 69.3626° |
| perigee height: | 975 km |
| apogee height: | 1216 km |
| right ascension of ascending node: | 331.9845° |
| argument of perigee: | 37.1568° |
| revolutions per day: | 13.43655308 |
| mean anomaly at epoch: | 113.9854° |
| orbit number at epoch: | 24533 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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