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 24279.15170431 .00000077 00000-0 48566-3 0 9998
2 39485 82.4866 194.6102 0022159 24.0879 336.1232 12.42900074489063
| Epoch (UTC): | 05 October 2024 03:38:27 |
| Eccentricity: | 0.0022159 |
| inclination: | 82.4866° |
| perigee height: | 1477 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 194.6102° |
| argument of perigee: | 24.0879° |
| revolutions per day: | 12.42900074 |
| mean anomaly at epoch: | 336.1232° |
| orbit number at epoch: | 48906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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