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 39849U 92093LB 24354.13508407 .00001549 00000-0 95840-3 0 9990
2 39849 70.8666 271.4802 0085722 305.1327 54.1777 14.05060618540514
| Epoch (UTC): | 19 December 2024 03:14:31 |
| Eccentricity: | 0.0085722 |
| inclination: | 70.8666° |
| perigee height: | 814 km |
| apogee height: | 938 km |
| right ascension of ascending node: | 271.4802° |
| argument of perigee: | 305.1327° |
| revolutions per day: | 14.05060618 |
| mean anomaly at epoch: | 54.1777° |
| orbit number at epoch: | 54051 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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