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 40032U 14033Y 23332.41718683 .00007776 00000-0 71274-3 0 9992
2 40032 97.9856 275.4101 0012202 103.5662 256.6918 14.95138849512495
| Epoch (UTC): | 28 November 2023 10:00:44 |
| Eccentricity: | 0.0012202 |
| inclination: | 97.9856° |
| perigee height: | 573 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 275.4101° |
| argument of perigee: | 103.5662° |
| revolutions per day: | 14.95138849 |
| mean anomaly at epoch: | 256.6918° |
| orbit number at epoch: | 51249 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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