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 40018U 14033J 23083.69564611 .00001680 00000-0 27263-3 0 9996
2 40018 97.7420 244.7371 0071150 34.7071 325.8748 14.70747055469969
| Epoch (UTC): | 24 March 2023 16:41:43 |
| Eccentricity: | 0.0071150 |
| inclination: | 97.7420° |
| perigee height: | 608 km |
| apogee height: | 709 km |
| right ascension of ascending node: | 244.7371° |
| argument of perigee: | 34.7071° |
| revolutions per day: | 14.70747055 |
| mean anomaly at epoch: | 325.8748° |
| orbit number at epoch: | 46996 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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