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 24260.81127090 .00012130 00000-0 13723-2 0 9993
2 39440 97.8174 202.5998 0066876 336.3856 23.4292 14.84961890581927
| Epoch (UTC): | 16 September 2024 19:28:13 |
| Eccentricity: | 0.0066876 |
| inclination: | 97.8174° |
| perigee height: | 567 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 202.5998° |
| argument of perigee: | 336.3856° |
| revolutions per day: | 14.84961890 |
| mean anomaly at epoch: | 23.4292° |
| orbit number at epoch: | 58192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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