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 68117U 26145.41678867 +.00000000 +00000-0 +59576-3 0 00006
2 68117 97.2845 106.0732 0001894 98.7266 261.4191 15.33445918 06
| Epoch (UTC): | 25 May 2026 10:00:10 |
| Eccentricity: | 0.0001894 |
| inclination: | 97.2845° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 106.0732° |
| argument of perigee: | 98.7266° |
| revolutions per day: | 15.33445918 |
| mean anomaly at epoch: | 261.4191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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