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 17191U 26102.84492291 +.00000000 +00000-0 +29091-3 0 00006
2 17191 82.4577 59.6730 0003889 64.7845 295.3808 15.49372674 09
| Epoch (UTC): | 12 April 2026 20:16:41 |
| Eccentricity: | 0.0003889 |
| inclination: | 82.4577° |
| perigee height: | 416 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 59.6730° |
| argument of perigee: | 64.7845° |
| revolutions per day: | 15.49372674 |
| mean anomaly at epoch: | 295.3808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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