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 26064.64689336 +.00000000 +00000-0 +13478-3 0 00003
2 26931 67.0508 152.0681 0007017 265.3192 94.7108 14.31909897 05
| Epoch (UTC): | 05 March 2026 15:31:31 |
| Eccentricity: | 0.0007017 |
| inclination: | 67.0508° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 152.0681° |
| argument of perigee: | 265.3192° |
| revolutions per day: | 14.31909897 |
| mean anomaly at epoch: | 94.7108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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