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 35686U 26145.16017667 +.00000000 +00000-0 +16813-3 0 00005
2 35686 98.2035 297.2866 0062710 142.3089 218.2549 14.96150176 01
| Epoch (UTC): | 25 May 2026 03:50:39 |
| Eccentricity: | 0.0062710 |
| inclination: | 98.2035° |
| perigee height: | 535 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 297.2866° |
| argument of perigee: | 142.3089° |
| revolutions per day: | 14.96150176 |
| mean anomaly at epoch: | 218.2549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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