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 20442U 26066.59765572 +.00000000 +00000-0 +93148-4 0 00000
2 20442 98.8937 85.5652 0012261 140.1670 220.0416 14.34087096 07
| Epoch (UTC): | 07 March 2026 14:20:37 |
| Eccentricity: | 0.0012261 |
| inclination: | 98.8937° |
| perigee height: | 769 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 85.5652° |
| argument of perigee: | 140.1670° |
| revolutions per day: | 14.34087096 |
| mean anomaly at epoch: | 220.0416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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