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 22566U 26017.25611132 +.00000000 +00000-0 -32954-5 0 00000
2 22566 71.0088 323.2086 0008810 30.4153 329.7479 14.15293380 01
| Epoch (UTC): | 17 January 2026 06:08:48 |
| Eccentricity: | 0.0008810 |
| inclination: | 71.0088° |
| perigee height: | 835 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 323.2086° |
| argument of perigee: | 30.4153° |
| revolutions per day: | 14.15293380 |
| mean anomaly at epoch: | 329.7479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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