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 26158.57486742 +.00000000 +00000-0 +38371-3 0 00002
2 20692 63.2941 235.6720 0873564 84.5192 285.4734 13.64655191 07
| Epoch (UTC): | 07 June 2026 13:47:48 |
| Eccentricity: | 0.0873564 |
| inclination: | 63.2941° |
| perigee height: | 373 km |
| apogee height: | 1665 km |
| right ascension of ascending node: | 235.6720° |
| argument of perigee: | 84.5192° |
| revolutions per day: | 13.64655191 |
| mean anomaly at epoch: | 285.4734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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