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 68869U 26145.50003470 +.00000000 +00000-0 -13451+0 0 00001
2 68869 51.8851 354.2896 0007668 237.2648 351.2937 15.05276979 04
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0007668 |
| inclination: | 51.8851° |
| perigee height: | 545 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 354.2896° |
| argument of perigee: | 237.2648° |
| revolutions per day: | 15.05276979 |
| mean anomaly at epoch: | 351.2937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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