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 43803U 18099AX 24251.68922772 .00026012 00000-0 16056-2 0 9993
2 43803 97.5119 308.6109 0009404 29.0354 331.1397 15.09843342315138
| Epoch (UTC): | 07 September 2024 16:32:29 |
| Eccentricity: | 0.0009404 |
| inclination: | 97.5119° |
| perigee height: | 530 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 308.6109° |
| argument of perigee: | 29.0354° |
| revolutions per day: | 15.09843342 |
| mean anomaly at epoch: | 331.1397° |
| orbit number at epoch: | 31513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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