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 26155.27473536 +.00000000 +00000-0 +70342-4 0 00001
2 20442 98.8853 176.7242 0010549 241.5531 118.4591 14.34119202 00
| Epoch (UTC): | 04 June 2026 06:35:37 |
| Eccentricity: | 0.0010549 |
| inclination: | 98.8853° |
| perigee height: | 770 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 176.7242° |
| argument of perigee: | 241.5531° |
| revolutions per day: | 14.34119202 |
| mean anomaly at epoch: | 118.4591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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