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 26065.29795399 +.00000000 +00000-0 +64170-4 0 00008
2 17526 82.9045 179.9619 0041134 55.1227 305.3786 13.77212018 02
| Epoch (UTC): | 06 March 2026 07:09:03 |
| Eccentricity: | 0.0041134 |
| inclination: | 82.9045° |
| perigee height: | 944 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 179.9619° |
| argument of perigee: | 55.1227° |
| revolutions per day: | 13.77212018 |
| mean anomaly at epoch: | 305.3786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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