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 41607U 16040J 23229.04174353 .13176613 23928-5 47180-3 0 9994
2 41607 97.1092 282.4108 0013403 255.3735 104.6081 16.43046180398647
| Epoch (UTC): | 17 August 2023 01:00:06 |
| Eccentricity: | 0.0013403 |
| inclination: | 97.1092° |
| perigee height: | 149 km |
| apogee height: | 166 km |
| right ascension of ascending node: | 282.4108° |
| argument of perigee: | 255.3735° |
| revolutions per day: | 16.43046180 |
| mean anomaly at epoch: | 104.6081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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