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 65818U 26145.49225376 +.00000000 +00000-0 +56942-4 0 00007
2 65818 86.5007 51.5691 0001355 66.8661 293.2616 13.24406233 07
| Epoch (UTC): | 25 May 2026 11:48:50 |
| Eccentricity: | 0.0001355 |
| inclination: | 86.5007° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 51.5691° |
| argument of perigee: | 66.8661° |
| revolutions per day: | 13.24406233 |
| mean anomaly at epoch: | 293.2616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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