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 26140.44434753 +.00000000 +00000-0 +66113-4 0 00002
2 18822 98.3550 308.2046 0007110 143.0887 217.0786 14.28817459 06
| Epoch (UTC): | 20 May 2026 10:39:51 |
| Eccentricity: | 0.0007110 |
| inclination: | 98.3550° |
| perigee height: | 791 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 308.2046° |
| argument of perigee: | 143.0887° |
| revolutions per day: | 14.28817459 |
| mean anomaly at epoch: | 217.0786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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