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 17526U 26046.84448823 +.00000000 +00000-0 -12479-4 0 00001
2 17526 82.9019 193.7559 0041467 105.1424 255.4326 13.77210966 09
| Epoch (UTC): | 15 February 2026 20:16:03 |
| Eccentricity: | 0.0041467 |
| inclination: | 82.9019° |
| perigee height: | 943 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 193.7559° |
| argument of perigee: | 105.1424° |
| revolutions per day: | 13.77210966 |
| mean anomaly at epoch: | 255.4326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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