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 24258.58760468 .00018301 00000-0 20672-2 0 9993
2 39440 97.8165 200.4175 0067176 343.7204 16.1852 14.84912339581592
| Epoch (UTC): | 14 September 2024 14:06:09 |
| Eccentricity: | 0.0067176 |
| inclination: | 97.8165° |
| perigee height: | 567 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 200.4175° |
| argument of perigee: | 343.7204° |
| revolutions per day: | 14.84912339 |
| mean anomaly at epoch: | 16.1852° |
| orbit number at epoch: | 58159 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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