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 22078U 26106.54605794 +.00000000 +00000-0 -54989-4 0 00007
2 22078 66.0873 37.6382 0015776 296.6275 63.3127 12.86851631 06
| Epoch (UTC): | 16 April 2026 13:06:19 |
| Eccentricity: | 0.0015776 |
| inclination: | 66.0873° |
| perigee height: | 1302 km |
| apogee height: | 1326 km |
| right ascension of ascending node: | 37.6382° |
| argument of perigee: | 296.6275° |
| revolutions per day: | 12.86851631 |
| mean anomaly at epoch: | 63.3127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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