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 40046U 14033AN 23083.50009410 .00010511 00000-0 14063-2 0 9994
2 40046 97.6516 270.8027 0053176 312.3510 47.3204 14.78649692471517
| Epoch (UTC): | 24 March 2023 12:00:08 |
| Eccentricity: | 0.0053176 |
| inclination: | 97.6516° |
| perigee height: | 596 km |
| apogee height: | 671 km |
| right ascension of ascending node: | 270.8027° |
| argument of perigee: | 312.3510° |
| revolutions per day: | 14.78649692 |
| mean anomaly at epoch: | 47.3204° |
| orbit number at epoch: | 47151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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