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 39440U 13066AA 24280.61892180 .00014851 00000-0 16614-2 0 9996
2 39440 97.8208 222.0492 0065015 269.6478 89.7287 14.85458730586067
| Epoch (UTC): | 06 October 2024 14:51:14 |
| Eccentricity: | 0.0065015 |
| inclination: | 97.8208° |
| perigee height: | 567 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 222.0492° |
| argument of perigee: | 269.6478° |
| revolutions per day: | 14.85458730 |
| mean anomaly at epoch: | 89.7287° |
| orbit number at epoch: | 58606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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