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 26106.84737854 +.00000000 +00000-0 +38153-4 0 00009
2 20441 98.8785 133.6907 0011906 45.3555 128.8289 14.33974171 09
| Epoch (UTC): | 16 April 2026 20:20:13 |
| Eccentricity: | 0.0011906 |
| inclination: | 98.8785° |
| perigee height: | 770 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 133.6907° |
| argument of perigee: | 45.3555° |
| revolutions per day: | 14.33974171 |
| mean anomaly at epoch: | 128.8289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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