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 20691U 26159.45285409 +.00000000 +00000-0 +21445-3 0 00000
2 20691 63.2936 235.3739 0880647 85.0079 285.0775 13.62738329 01
| Epoch (UTC): | 08 June 2026 10:52:06 |
| Eccentricity: | 0.0880647 |
| inclination: | 63.2936° |
| perigee height: | 374 km |
| apogee height: | 1678 km |
| right ascension of ascending node: | 235.3739° |
| argument of perigee: | 85.0079° |
| revolutions per day: | 13.62738329 |
| mean anomaly at epoch: | 285.0775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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