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 17567U 26044.66888333 +.00000000 +00000-0 +50935-4 0 00006
2 17567 82.5283 115.3416 0017715 345.1544 14.9149 14.86109022 05
| Epoch (UTC): | 13 February 2026 16:03:11 |
| Eccentricity: | 0.0017715 |
| inclination: | 82.5283° |
| perigee height: | 598 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 115.3416° |
| argument of perigee: | 345.1544° |
| revolutions per day: | 14.86109022 |
| mean anomaly at epoch: | 14.9149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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