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 43931U 19002K 24280.65706492 .00001923 00000-0 67935-3 0 9995
2 43931 86.3932 252.0300 0002406 87.9310 272.2161 14.34225161300301
| Epoch (UTC): | 06 October 2024 15:46:10 |
| Eccentricity: | 0.0002406 |
| inclination: | 86.3932° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 252.0300° |
| argument of perigee: | 87.9310° |
| revolutions per day: | 14.34225161 |
| mean anomaly at epoch: | 272.2161° |
| orbit number at epoch: | 30030 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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