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 26156.32126850 +.00000000 +00000-0 +61458-4 0 00000
2 20442 98.8853 177.7996 0010571 238.2188 121.7967 14.34119464 07
| Epoch (UTC): | 05 June 2026 07:42:37 |
| Eccentricity: | 0.0010571 |
| inclination: | 98.8853° |
| perigee height: | 770 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 177.7996° |
| argument of perigee: | 238.2188° |
| revolutions per day: | 14.34119464 |
| mean anomaly at epoch: | 121.7967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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