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 23340.38084637 .00005518 00000-0 50590-3 0 9992
2 40032 97.9847 283.5192 0012062 82.0088 278.2500 14.95265516513683
| Epoch (UTC): | 06 December 2023 09:08:25 |
| Eccentricity: | 0.0012062 |
| inclination: | 97.9847° |
| perigee height: | 573 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 283.5192° |
| argument of perigee: | 82.0088° |
| revolutions per day: | 14.95265516 |
| mean anomaly at epoch: | 278.2500° |
| orbit number at epoch: | 51368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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