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 39485U 13076C 24259.91312534 .00000032 00000-0 16010-3 0 9992
2 39485 82.4844 206.5942 0022559 64.3590 295.9817 12.42898654486467
| Epoch (UTC): | 15 September 2024 21:54:54 |
| Eccentricity: | 0.0022559 |
| inclination: | 82.4844° |
| perigee height: | 1476 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 206.5942° |
| argument of perigee: | 64.3590° |
| revolutions per day: | 12.42898654 |
| mean anomaly at epoch: | 295.9817° |
| orbit number at epoch: | 48646 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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