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 23339.51089703 .00005850 00000-0 53611-3 0 9990
2 40032 97.9846 282.6332 0012014 84.2621 275.9969 14.95255913513551
| Epoch (UTC): | 05 December 2023 12:15:41 |
| Eccentricity: | 0.0012014 |
| inclination: | 97.9846° |
| perigee height: | 573 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 282.6332° |
| argument of perigee: | 84.2621° |
| revolutions per day: | 14.95255913 |
| mean anomaly at epoch: | 275.9969° |
| orbit number at epoch: | 51355 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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