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 26145.38964784 +.00000000 +00000-0 +74589-4 0 00008
2 26931 67.0508 303.2359 0006184 263.8379 96.2019 14.31946061 03
| Epoch (UTC): | 25 May 2026 09:21:05 |
| Eccentricity: | 0.0006184 |
| inclination: | 67.0508° |
| perigee height: | 781 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 303.2359° |
| argument of perigee: | 263.8379° |
| revolutions per day: | 14.31946061 |
| mean anomaly at epoch: | 96.2019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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