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 26064.61647735 +.00000000 +00000-0 +29358-3 0 00008
2 20691 63.2940 131.0472 0883013 83.1632 286.8940 13.61935163 03
| Epoch (UTC): | 05 March 2026 14:47:43 |
| Eccentricity: | 0.0883013 |
| inclination: | 63.2940° |
| perigee height: | 375 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 131.0472° |
| argument of perigee: | 83.1632° |
| revolutions per day: | 13.61935163 |
| mean anomaly at epoch: | 286.8940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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