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 26022.33332381 +.00000000 +00000-0 +12244-3 0 00009
2 20046 82.9380 121.4798 0040647 257.3380 102.3232 13.78605772 04
| Epoch (UTC): | 22 January 2026 07:59:59 |
| Eccentricity: | 0.0040647 |
| inclination: | 82.9380° |
| perigee height: | 939 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 121.4798° |
| argument of perigee: | 257.3380° |
| revolutions per day: | 13.78605772 |
| mean anomaly at epoch: | 102.3232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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