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 is defined by the following mean orbital elements,
1 41732U 16051B 23352.62592397 .15255748 24834-5 15674-3 0 9997
2 41732 97.3647 294.9317 0008647 58.0049 302.2095 16.50692741410424
| Epoch (UTC): | 18 December 2023 15:01:19 |
| Eccentricity: | 0.0008647 |
| inclination: | 97.3647° |
| perigee height: | 132 km |
| apogee height: | 143 km |
| right ascension of ascending node: | 294.9317° |
| argument of perigee: | 58.0049° |
| revolutions per day: | 16.50692741 |
| mean anomaly at epoch: | 302.2095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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