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 22565U 26156.87411937 +.00000000 +00000-0 +25050-4 0 00009
2 22565 70.7610 336.7998 0008968 271.8782 88.1310 14.12366640 08
| Epoch (UTC): | 05 June 2026 20:58:43 |
| Eccentricity: | 0.0008968 |
| inclination: | 70.7610° |
| perigee height: | 845 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 336.7998° |
| argument of perigee: | 271.8782° |
| revolutions per day: | 14.12366640 |
| mean anomaly at epoch: | 88.1310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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