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 26065.37060524 +.00000000 +00000-0 +64015-4 0 00000
2 17526 82.9045 179.9076 0041131 54.9245 305.5759 13.77212029 07
| Epoch (UTC): | 06 March 2026 08:53:40 |
| Eccentricity: | 0.0041131 |
| inclination: | 82.9045° |
| perigee height: | 944 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 179.9076° |
| argument of perigee: | 54.9245° |
| revolutions per day: | 13.77212029 |
| mean anomaly at epoch: | 305.5759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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