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 24262.81436213 .00011351 00000-0 89888-3 0 9999
2 40032 98.0120 217.8898 0009110 162.4375 197.7165 15.00729480557226
| Epoch (UTC): | 18 September 2024 19:32:40 |
| Eccentricity: | 0.0009110 |
| inclination: | 98.0120° |
| perigee height: | 558 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 217.8898° |
| argument of perigee: | 162.4375° |
| revolutions per day: | 15.00729480 |
| mean anomaly at epoch: | 197.7165° |
| orbit number at epoch: | 55722 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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