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 18822U 26146.18665319 +.00000000 +00000-0 +10994-3 0 00008
2 18822 98.3554 313.7060 0007349 128.2941 231.8904 14.28820303 05
| Epoch (UTC): | 26 May 2026 04:28:46 |
| Eccentricity: | 0.0007349 |
| inclination: | 98.3554° |
| perigee height: | 790 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 313.7060° |
| argument of perigee: | 128.2941° |
| revolutions per day: | 14.28820303 |
| mean anomaly at epoch: | 231.8904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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