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 43017U 17073E 24340.15469960 .00014443 00000-0 79797-3 0 9994
2 43017 97.5487 209.9561 0194773 79.3473 282.9618 14.99180602381225
| Epoch (UTC): | 05 December 2024 03:42:46 |
| Eccentricity: | 0.0194773 |
| inclination: | 97.5487° |
| perigee height: | 434 km |
| apogee height: | 705 km |
| right ascension of ascending node: | 209.9561° |
| argument of perigee: | 79.3473° |
| revolutions per day: | 14.99180602 |
| mean anomaly at epoch: | 282.9618° |
| orbit number at epoch: | 38122 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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