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 26021.53496404 +.00000000 +00000-0 +10427-3 0 00008
2 20046 82.9380 122.0752 0040651 259.6653 99.9921 13.78605436 07
| Epoch (UTC): | 21 January 2026 12:50:20 |
| Eccentricity: | 0.0040651 |
| inclination: | 82.9380° |
| perigee height: | 939 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 122.0752° |
| argument of perigee: | 259.6653° |
| revolutions per day: | 13.78605436 |
| mean anomaly at epoch: | 99.9921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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