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 20046U 26017.68832131 +.00000000 +00000-0 +20989-4 0 00005
2 20046 82.9381 124.9437 0040612 270.8179 88.8326 13.78604564 01
| Epoch (UTC): | 17 January 2026 16:31:10 |
| Eccentricity: | 0.0040612 |
| inclination: | 82.9381° |
| perigee height: | 939 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 124.9437° |
| argument of perigee: | 270.8179° |
| revolutions per day: | 13.78604564 |
| mean anomaly at epoch: | 88.8326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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