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 68009U 26145.51717647 +.00000000 +00000-0 +78697-3 0 00002
2 68009 43.0018 335.0102 0002067 275.3195 84.7421 15.27591708 03
| Epoch (UTC): | 25 May 2026 12:24:44 |
| Eccentricity: | 0.0002067 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 335.0102° |
| argument of perigee: | 275.3195° |
| revolutions per day: | 15.27591708 |
| mean anomaly at epoch: | 84.7421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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