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 40746U 15036A 23274.19979972 .00000007 00000-0 00000+0 0 9993
2 40746 0.0124 228.3915 0000230 314.8339 73.4037 1.00270701 29942
| Epoch (UTC): | 01 October 2023 04:47:42 |
| Eccentricity: | 0.0000230 |
| inclination: | 0.0124° |
| perigee height: | 35785 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 228.3915° |
| argument of perigee: | 314.8339° |
| revolutions per day: | 1.00270701 |
| mean anomaly at epoch: | 73.4037° |
| orbit number at epoch: | 2994 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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