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 26066.18354100 +.00000000 +00000-0 +10989-3 0 00006
2 26931 67.0508 148.0942 0007005 265.2738 94.7564 14.31910626 00
| Epoch (UTC): | 07 March 2026 04:24:17 |
| Eccentricity: | 0.0007005 |
| inclination: | 67.0508° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 148.0942° |
| argument of perigee: | 265.2738° |
| revolutions per day: | 14.31910626 |
| mean anomaly at epoch: | 94.7564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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