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 23079.67466659 .00011744 00000-0 83587-3 0 9994
2 43017 97.6440 327.5263 0238185 1.6676 358.5279 14.84658553288048
| Epoch (UTC): | 20 March 2023 16:11:31 |
| Eccentricity: | 0.0238185 |
| inclination: | 97.6440° |
| perigee height: | 448 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 327.5263° |
| argument of perigee: | 1.6676° |
| revolutions per day: | 14.84658553 |
| mean anomaly at epoch: | 358.5279° |
| orbit number at epoch: | 28804 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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