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 24259.80052347 .00014189 00000-0 16043-2 0 9996
2 39440 97.8170 201.6077 0067009 339.7487 20.1072 14.84939882581776
| Epoch (UTC): | 15 September 2024 19:12:45 |
| Eccentricity: | 0.0067009 |
| inclination: | 97.8170° |
| perigee height: | 567 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 201.6077° |
| argument of perigee: | 339.7487° |
| revolutions per day: | 14.84939882 |
| mean anomaly at epoch: | 20.1072° |
| orbit number at epoch: | 58177 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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