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 20692U 26140.40037444 +.00000000 +00000-0 +35824-3 0 00006
2 20692 63.2944 284.8389 0874585 84.1754 285.8188 13.64427987 08
| Epoch (UTC): | 20 May 2026 09:36:32 |
| Eccentricity: | 0.0874585 |
| inclination: | 63.2944° |
| perigee height: | 373 km |
| apogee height: | 1667 km |
| right ascension of ascending node: | 284.8389° |
| argument of perigee: | 84.1754° |
| revolutions per day: | 13.64427987 |
| mean anomaly at epoch: | 285.8188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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