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 24280.90990684 .00028535 00000-0 16560-2 0 9997
2 43017 97.5553 152.5667 0198583 279.3630 78.5189 14.96920568372355
| Epoch (UTC): | 06 October 2024 21:50:15 |
| Eccentricity: | 0.0198583 |
| inclination: | 97.5553° |
| perigee height: | 438 km |
| apogee height: | 714 km |
| right ascension of ascending node: | 152.5667° |
| argument of perigee: | 279.3630° |
| revolutions per day: | 14.96920568 |
| mean anomaly at epoch: | 78.5189° |
| orbit number at epoch: | 37235 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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