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 40042U 14033AJ 23333.41248255 .00012134 00000-0 10398-2 0 9990
2 40042 98.0286 285.9369 0014358 95.7301 264.5557 14.97616177512745
| Epoch (UTC): | 29 November 2023 09:53:58 |
| Eccentricity: | 0.0014358 |
| inclination: | 98.0286° |
| perigee height: | 564 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 285.9369° |
| argument of perigee: | 95.7301° |
| revolutions per day: | 14.97616177 |
| mean anomaly at epoch: | 264.5557° |
| orbit number at epoch: | 51274 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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