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 26071.76391156 +.00000000 +00000-0 +52687-4 0 00000
2 17526 82.9049 175.1294 0040790 37.3826 323.0157 13.77212792 05
| Epoch (UTC): | 12 March 2026 18:20:01 |
| Eccentricity: | 0.0040790 |
| inclination: | 82.9049° |
| perigee height: | 944 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 175.1294° |
| argument of perigee: | 37.3826° |
| revolutions per day: | 13.77212792 |
| mean anomaly at epoch: | 323.0157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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