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 24257.37466015 .00021961 00000-0 24798-2 0 9999
2 39440 97.8159 199.2275 0067392 347.6795 12.2768 14.84874160582615
| Epoch (UTC): | 13 September 2024 08:59:30 |
| Eccentricity: | 0.0067392 |
| inclination: | 97.8159° |
| perigee height: | 567 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 199.2275° |
| argument of perigee: | 347.6795° |
| revolutions per day: | 14.84874160 |
| mean anomaly at epoch: | 12.2768° |
| orbit number at epoch: | 58261 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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