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 is defined by the following mean orbital elements,
1 43017U 26046.07360744 +.00000000 +00000-0 +34084-3 0 00009
2 43017 97.4901 275.8509 0158012 30.0352 330.9825 15.10338894 05
| Epoch (UTC): | 15 February 2026 01:45:59 |
| Eccentricity: | 0.0158012 |
| inclination: | 97.4901° |
| perigee height: | 426 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 275.8509° |
| argument of perigee: | 30.0352° |
| revolutions per day: | 15.10338894 |
| mean anomaly at epoch: | 330.9825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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