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 26101.27336072 +.00000000 +00000-0 +56682-4 0 00006
2 20442 98.8904 121.2198 0012344 46.5826 313.6383 14.34102144 02
| Epoch (UTC): | 11 April 2026 06:33:38 |
| Eccentricity: | 0.0012344 |
| inclination: | 98.8904° |
| perigee height: | 769 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 121.2198° |
| argument of perigee: | 46.5826° |
| revolutions per day: | 14.34102144 |
| mean anomaly at epoch: | 313.6383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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