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 26931U 26065.62476010 +.00000000 +00000-0 +12745-3 0 00001
2 26931 67.0508 149.5392 0007016 265.2992 94.7308 14.31910487 00
| Epoch (UTC): | 06 March 2026 14:59:39 |
| Eccentricity: | 0.0007016 |
| inclination: | 67.0508° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 149.5392° |
| argument of perigee: | 265.2992° |
| revolutions per day: | 14.31910487 |
| mean anomaly at epoch: | 94.7308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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