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 20706U 26150.48908469 +.00000000 +00000-0 +00000-0 0 00000
2 20706 14.5666 3.7774 0005857 276.6837 72.4873 0.99546968 04
| Epoch (UTC): | 30 May 2026 11:44:16 |
| Eccentricity: | 0.0005857 |
| inclination: | 14.5666° |
| perigee height: | 35966 km |
| apogee height: | 36016 km |
| right ascension of ascending node: | 3.7774° |
| argument of perigee: | 276.6837° |
| revolutions per day: | 0.99546968 |
| mean anomaly at epoch: | 72.4873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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