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 22175U 26149.74617059 +.00000000 +00000-0 +00000-0 0 00001
2 22175 14.2337 7.2031 0000477 104.9391 67.0040 0.99732349 00
| Epoch (UTC): | 29 May 2026 17:54:29 |
| Eccentricity: | 0.0000477 |
| inclination: | 14.2337° |
| perigee height: | 35936 km |
| apogee height: | 35941 km |
| right ascension of ascending node: | 7.2031° |
| argument of perigee: | 104.9391° |
| revolutions per day: | 0.99732349 |
| mean anomaly at epoch: | 67.0040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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