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 26064.71674390 +.00000000 +00000-0 +47116-4 0 00002
2 17526 82.9045 180.3964 0041137 56.6905 303.8181 13.77211824 09
| Epoch (UTC): | 05 March 2026 17:12:06 |
| Eccentricity: | 0.0041137 |
| inclination: | 82.9045° |
| perigee height: | 944 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 180.3964° |
| argument of perigee: | 56.6905° |
| revolutions per day: | 13.77211824 |
| mean anomaly at epoch: | 303.8181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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