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 18350U 26151.31997191 +.00000000 +00000-0 +00000-0 0 00005
2 18350 14.3919 351.3635 0005960 15.5598 161.5174 0.98909268 01
| Epoch (UTC): | 31 May 2026 07:40:45 |
| Eccentricity: | 0.0005960 |
| inclination: | 14.3919° |
| perigee height: | 36148 km |
| apogee height: | 36198 km |
| right ascension of ascending node: | 351.3635° |
| argument of perigee: | 15.5598° |
| revolutions per day: | 0.98909268 |
| mean anomaly at epoch: | 161.5174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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