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 20440U 26112.04689381 +.00000000 +00000-0 +47611-4 0 00007
2 20440 98.8662 141.0238 0010740 16.3813 12.0051 14.34470148 09
| Epoch (UTC): | 22 April 2026 01:07:31 |
| Eccentricity: | 0.0010740 |
| inclination: | 98.8662° |
| perigee height: | 769 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 141.0238° |
| argument of perigee: | 16.3813° |
| revolutions per day: | 14.34470148 |
| mean anomaly at epoch: | 12.0051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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