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 20441U 26110.30449419 +.00000000 +00000-0 +34891-4 0 00007
2 20441 98.8780 137.2395 0011753 35.8781 334.8660 14.33974846 01
| Epoch (UTC): | 20 April 2026 07:18:28 |
| Eccentricity: | 0.0011753 |
| inclination: | 98.8780° |
| perigee height: | 770 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 137.2395° |
| argument of perigee: | 35.8781° |
| revolutions per day: | 14.33974846 |
| mean anomaly at epoch: | 334.8660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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