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 68110U 26145.37329867 +.00000000 +00000-0 +93722-3 0 00008
2 68110 97.2837 105.9768 0001129 86.4543 273.6829 15.33433737 09
| Epoch (UTC): | 25 May 2026 08:57:33 |
| Eccentricity: | 0.0001129 |
| inclination: | 97.2837° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 105.9768° |
| argument of perigee: | 86.4543° |
| revolutions per day: | 15.33433737 |
| mean anomaly at epoch: | 273.6829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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