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 26053.66660153 +.00000000 +00000-0 +55210-4 0 00000
2 20441 98.8858 79.0815 0010993 191.6021 284.8168 14.33954124 04
| Epoch (UTC): | 22 February 2026 15:59:54 |
| Eccentricity: | 0.0010993 |
| inclination: | 98.8858° |
| perigee height: | 771 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 79.0815° |
| argument of perigee: | 191.6021° |
| revolutions per day: | 14.33954124 |
| mean anomaly at epoch: | 284.8168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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