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 44547U 19063A 24358.49313219 .00000577 00000-0 22577-3 0 9992
2 44547 98.4336 12.9647 0006117 348.4950 11.6094 14.33143888274441
| Epoch (UTC): | 23 December 2024 11:50:06 |
| Eccentricity: | 0.0006117 |
| inclination: | 98.4336° |
| perigee height: | 777 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 12.9647° |
| argument of perigee: | 348.4950° |
| revolutions per day: | 14.33143888 |
| mean anomaly at epoch: | 11.6094° |
| orbit number at epoch: | 27444 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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