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 26069.94663594 +.00000000 +00000-0 +80767-4 0 00006
2 20442 98.8937 89.0093 0012385 130.9647 229.2611 14.34088549 05
| Epoch (UTC): | 10 March 2026 22:43:09 |
| Eccentricity: | 0.0012385 |
| inclination: | 98.8937° |
| perigee height: | 769 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 89.0093° |
| argument of perigee: | 130.9647° |
| revolutions per day: | 14.34088549 |
| mean anomaly at epoch: | 229.2611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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